N374FE, cancelled Mar 22, 2017

Service difficulty reports · 46

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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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 n_number = 'N374FE' AND deregistration_id = 'N374FE-2017-03-22'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA00738Reducer · leakingHYD 3 ELEV OFF AND HYD 3 QTY LOW ALERT ANNUNCIATED. HYDRAULIC QUANTITY STABILIZED AT 3.9 GALLON. TIGHTENED "B" NUT UNION (REDUCER) ON RT MAIN LANDING GEAR SWIVEL GLAND, SERVICED HYDRAULICS'S AND LEAK CHECKED CHECKED GOOD IAW MD10-10 AMM 20-50-01-2 AND MD10-Mar 5, 2008 · N374FE · Doug MD1010F · Hydraulic System, MainSDR 08FDEA00522Intercostal · corrodedLOWER AFT CARGO COMPARTMENT CORROSION ON INTERCOSTAL BETWEEN STRINGERS 44 AND 45 LT AT FS 1781. FABRICATED NEW INTERCOSTAL PER DAC DAW AFA 3870 REV F AND INSTALLED PER DC/MD10 SRM 51-33-01 VOL II.Feb 20, 2008 · N374FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR 08FDEA00515Skin · corrodedCENTER WHEEL WELL LOWER SKIN HAS CORROSION FROM FS 1501 TO 1521 BETWEEN STR 50L TO51R. REMOVED, FABRICATED AND INSTALLED REPAIR PER E8-5330-113024" FUSELAGE-SKIN AT STA 1519 AND L-52-REPAIR.Feb 19, 2008 · N374FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 08FDEA00450Web · crackedCENTER CARGO COMP AT STA 1781 BELOW THE FLOOR AREA FROM L 52 - L 44 L WEB P/N AFA0154-5 1S CRACKED. FABRICATED NEW WEB PER REF. DAC DWG AFA 0154 REV. AT. INSTALLED IAW MD/DC 10 SRM 51-33-01 VOL. II. PART MARKED PER GMM7-0-1000. MINOR REPAIR.Feb 15, 2008 · N374FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR 08FDEA00449Skin · corrodedCENTER WHEEL WELL LOWER INTERIOR SKIN HAS CORROSION BETWEEN STR 47 R AND STR 48 R FROM FS 1501 TO FS 1520. REMOVED, FABRICATED AND INSTALLED REPAIR PER E8-5330-113023 "FUSELAGE-SKIN AT STA 1507 AND 1519 AND L-48 RT-REPAIR.Feb 15, 2008 · N374FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 08FDEA00451Skin · corrodedRIGHT WING UPPER TRAILING EDGE PANEL HAS CORROSION ON THE UPPER SURFACE, APPROXIMATELY XORS 345. REMOVED CORROSION; OUT OF LIMITS IAW 10 SRM 51-21-01, VOL II & 57-31-01 FIG A, VOL III & 57-00-01 FIG A, VOL I. REMOVED PANEL IAW SRM 51-33-01, VOL II, 51-3Feb 15, 2008 · N374FE · Doug MD1010F · Wing, Plate/SkinSDR 08FDEA00339Shear Tie · damagedFWD PIT AT STA 808 BETWEEN STR 42L AND STR 43L SHEARTIE HAS TOOL MARKS. FABBED NEW SHEARTIE IN REF TO FEDEX GMM 7-0-1001 AND DAC DWG RAM1470. REMOVED AND INSTALLED SHEARTIE AT STA 808 L42L - L43L IN REF TO DC/MD10-10 SRM 51-33-01 VOL II PG1.Jan 31, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA00328Skin · misrepairedFOUND REPAIR DOUBLER R/W O/B FLAP LOWER SKIN STA XOF 458. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NOT TO BE WITHIN THE LIMITS OF DC/MD10 SRM 57-10-00 FIG9 VJan 30, 2008 · N374FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA00329Skin · failedLT I/B FLAP LOWER EXTERNAL SURFACE HAS ERRODED DENT FILLER. REMOVED FILLER,FABRICATED AND INSTALLED NEW REPAIR IAW MD/DC10 SRM 57-10-00 FIG 85 VOLI , 51-21-01 VOLII.Jan 30, 2008 · N374FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA00315Angle · corrodedLWW, SLANT BULKHEAD PANEL LWR ATTACH ANGLE CORRODED AT SEVERAL AREAS BET LT AND RT CORNERS, FWD AND AFT FACES, STA 1381. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW MD/DC 10SRM 53-00-01 FIG 1A VOL I. MACHINED NEW SETION DWG APB7080 REV. D. INSTALLED PER Jan 28, 2008 · N374FE · Doug MD1010F · Fuselage Main, BulkheadSDR 08FDEA00313Skin · corrodedLWW, UPPER CTR TANK SKIN CORRODED, STA 1381, LBL 49. REMOVED AND REINSTALLED FASTENERS IAW SRM 51-31-01, VOL II. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01 FIG 1A VOL I, AND SRM 53-33-01 FIG 1 VOL III. ALODINED AND PRIMED IAW SRM 51-21-0Jan 28, 2008 · N374FE · Doug MD1010F · Fuel StorageSDR 08FDEA00311Skin · corrodedLWW, CTR TANK UPPER SKIN CORRODED STA 1381, LBL 76. REMOVED AND REINSTALLED FASTENERS IAW 51-31-01 VOL II. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01 FIG 1A VOL I AND SRM 57-33-01 FIG 1 VOL III. ALODINED AND PRIMED IAW SRM 51-21-01 VOL IIJan 28, 2008 · N374FE · Doug MD1010F · Fuel StorageSDR 08FDEA00281Floorbeam · corrodedFWD PIT AT STA 879 RBL 57 FLOORBEAM HAS CORROSION. FOUND TO BE OUT OF LIMITS AND REPAIRED BY SPLICING IN NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 VOL I FIG 7. THIS REPAIR IS CLASSIFIED AS MAJOR. ROLLER TRAY AT STA 765-879 RBL 56 REMOVED FOR ACCESS AND REINJan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Floor BeamSDR 08FDEA00280Frame · corrodedFWD PIT AT STA 919 BETWEEN STR 51R AND 51L LOWER FLANGE, FRAME HAS CORROSION. REPAIRED LOWER FLANGE AT STA 919, LONG 51R & 51L IAW DC/MD10-10 SRM 53-30-00, VOL I FIGURE 5Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, FrameSDR 08FDEA00282Door Frame · crackedNR 3 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHE (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00 PAGE 81 FIGURE 17 AT HOLE LOCATIONS A, B, C AND D TO CARGO DOOR Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00286Door Frame · crackedNR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00, PAGE 81 FIG 17 AT HOLE LOCATIONS A, C, AND D TO CARGO DOOR JAMB Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00285Door Frame · crackedNR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00, PAGE 81 FIG 17 AT HOLE LOCATIONS A, C, AND D TO CARGO DOOR JAMB Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00284Door Frame · crackedNR 4 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00 PAGE 81 FIG 17 AT HOLE LOCATIONS A, B, C AND D TO CARGO DOOR JAJan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00283Door Frame · crackedNR 1 MCD LOWER JAMB SUPPORT FITTING HOLE "C" HAS CRACK INDICATIONS, FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHING IN REFERENCE WITH DC/MD10-10 SRM VOLUME I 53-50-00 PAGE 81 FIG 17 AT HOLE LOCATION C, TO CARGO DOOR JAMB BEAM ONLY. LOWER FITJan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00276Shear Tie · damagedFWD PIT AT STA.808 BETWEEN STRINGER 34R AND 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED AND INSTALLED SHEAR TIE PER DC/MD10-10 SRM 53-13-01 VOL III FIG 8A AND 53-30-00 VOL I FIG10 AND 53-30-00 VOL I PAGE 34 FIG 9.Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA00245Shear Tie · corrodedLOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35L, SHEAR TIE HAS CORROSION ON LOWER FLANGE, PART ADA0003-19 REMOVED CORROSION IAW DC/MD10-10 SRM, VOLUME II, 51-21-01 PAGE 28. ORIGINAL THICKNESS IS .071 IAW DAC DWG ADA0003, REV M, PARTS LIST, ITEM -19. MATEJan 23, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA00222Frame · corrodedFOUND CORROSION ON FRAME LOWER SURFACE, FS 1099 BETWEEN L34L AND L35L. REMOVED CORROSION IAW SRM VOL II 51-21-01 PG 28A. FOUND TO BE OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 5 SHT 1. REMOVED AND REINSTALLED STRAP AND ANGLE IAW SRM VOLII 51-33-01. REMOVED Jan 22, 2008 · N374FE · Doug MD1010F · Fuselage Main, FrameSDR 08FDEA00210Shear Tie · corrodedCAC, CORROSION, SHEAR TIE, FS 1099 BETWEEN L51 R AND L50R REMOVED CORROSION IN REFERENCE WITH DC/MD10-10 SRM, VOLUME II, 51-21-01, PAGE 28A. ORIGINAL THICKNESS IA .071 INCH IAW DC/MD10-10 SRM, VOL III 53-13-01, FIGURE 8A, SHEET 1, ITEM 33. MATERIAL REMOVEDJan 21, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA00203Seat Track · gougedMCD STA 1239 RBL 48 SEAT TRACK GOUGED AND WORN EVALUATED SEAT TRACK; SEVERAL BROKEN SCALLOPS, OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED AND REINSTALLED 4 FLOOR PANELS AT STA 1199-1321 AND 1199-1259 RBL 27-76 IAW MD/DC 10-10 M/M 53-21-01-2Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00201Shear Tie · damagedFWD PIT AT STA 808 BETWEEN LONG 34R AND LONG 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED, AND INSTALLED SHER TIE PER SRM 53-13-01, VOL III FIG 8A AND SRM 53-30-00 VOL I FIG 10 AND SRM 53-30-00 VOL I PAGE 34 FIG 9 MAJOR REPAIR.Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA00200Shear Tie · corrodedLOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35, SHEAR TIE HAS CORROSION ON LOWER FLANGE. REMOVED CORROSION IAW SRM VOLUME II, 51-21-01 PAGE 28. FOUND TO BE OUT OF LIMITS IAW SRM, VOLUME I, 53-00-01, FIGURE 1B. FABRICATED NEW -19 IAW DAC DGW ADA0003Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA00198Support Fitting · crackedNR 2 MCD LOWER JAMB SUPPORT FITTING HOLES A, B AND C HAS CRACK INDICATIONS, FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS AT LOCATION NR 2 FITTING HOLES A, B AND C IAW SRM 53-50-00 VOL I PG 81 FIG 17.Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00195Support Fitting · crackedNR 5 MCD LOWER JAMB SUPPORT FITTING HOLES A AND D HAS CRACK INDICATIONS FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS IAW SRM 53-50-00 VOL I PG 81 FIG 17 AT NR 5 FITTING LOCATIONJan 18, 2008 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 08FDEA00159Fitting · crackedUPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 7 IS CRACKED IN HOLES "A, B, D" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 7 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage DoorsSDR 08FDEA00158Fitting · crackedUPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 6 IS CRACKED IN HOLE "A" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NUMBER 6 MAIN CARGO DOOR SPOOL LOCATION IN REF TO SRM 51-33-01 VOL II P/N AFA7132-1.Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage DoorsSDR 08FDEA00157Support Fitting · crackedUPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 4 IS CRACKED IN HOLES "A, C, D" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 4 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage DoorsSDR 08FDEA00156Support Fitting · crackedUPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 3 IS CRACKED IN HOLE "B" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NUMBER 3 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage DoorsSDR 08FDEA00155Support Fitting · crackedUPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 1 IS CRACKED IN HOLE "C" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 1 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage DoorsSDR 08FDEA00122Skin · cracked1 5/8" CRACK LOCATED ON THE RT HORIZONTAL STABILIZER AT THE INBOARD AFT CORNER OF THE OUTER SECTION UPPER AFT SKIN PANEL. END OF CRACK MARKED AND VERIFIED WITH HFEC INSPECTION. REPAIRED SKIN PLANK IAW EA 8-5510-116939, MAJOR REPAIR.Jan 14, 2008 · N374FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR 08FDEA00121Skin · crackedLT HORIZONTAL STAB UPPER REAR SKIN PANEL CRACKED, INITIATING FROM AFT EDGE OF SKIN AND PROCEDING FWD 21/4" (APPROXIMATELY). VERIFIED BY HFEC INSPECTION MARKED END OF CRACK. COMPLIED WITH AE 8-5510-116939. MAJOR REPAIR.Jan 14, 2008 · N374FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR 06FDEA3066Pressure Switch · failedNR 3 MANF FAIL INFLIGHT WHEN WING ANTI ICE SELECTED. FL340. COMPLIED WITH QRH. PERFORMED DECAY CHECK ON THE NR 3 MANIFOLD IAW MM 36-00-01-5, SYSTEM PASSED. CHECKED MANIFOLD FAIL DETECT UNIT IN CAC. FOUND RT WING PRESSURE SWITCH FAULTED. REMOVED AND REPLAAug 23, 2006 · N374FE · Doug MD1010F · Pneumatic Indicating SystemSDR 05FDEA00106Valve · malfunctionedENG 3 A-ICE DISAGREEMENT, LEVEL ONE ALERT ILLUMINATED STEADY WITH SWITCH IN EITHER POSITION. ENG NR 3 ANTI-ICE VALVE - INOP, FOUND OLD VALVE WAS BINDING SEVERLY AND DISAGREE LIGHT SWITCH WAS INOP ON VALVE. REMOVED AND REPLACED NR 3 NOSE COWL ANTI-ICE VALVE.Jan 17, 2005 · N374FE · Doug MD1010F · Air Intake Anti/De-Ice SystemSDR 05FDEA00043Skin · damagedNOT APPROVED FUSELAGE SKIN REPAIR AT LT AND RT LONG 44-47, STA 1526. SUBJECT REPAIRS WERE INSPECTED FOR COMPLIANCE WITH 14CFR 121.368, THE REPAIRS WERE EVALUATED TO BE ACCEPTABLE AS PERMANENT, PROVIDED REPAIRS ARE MODIFIED BY FEDEX EA 8-5310-84848.Aug 14, 2004 · N374FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 05FDEA00044Rail · corrodedBULK CARGO DOOR JAMB RAIL P/N AFA3249-1 CORRODED APPROX AT STA 1755-1764. FILLER, CAP AND REPAIR ANGLE INSTALLED AFTER CORROSION REMOVAL IAW FEDEX EA 8-5310- 79980.Jun 10, 2004 · N374FE · Doug MD1010F · Fuselage Main, StructureSDR 04FDEA00226Proximity Switch · faultyWHEN WE LOWERED THE GEAR FOR LANDING WE FELT THE GEAR COME DOWN BUT RED LIGHTS STAYED ON. WE MOVED THE HANDLE A FEW TIMES BUT NO HELP. RECYCLED GEAR AND THE RED LIGHTS STAYED ON. JIGGLED THE HANDLE AND THE LIGHTS FINALLY TURNED GREEN ALL AT THE SAME TIME.Jan 26, 2004 · N374FE · Doug DC1010 · Landing Gear Position and WarningSDR 03FDEA01681Switch · inoperativeAIR CONDITIONING DOORS LIGHT ON S/O PANEL BEGAN FLICKERING INFLIGHT. FUEL WAS DUMPED AND LANDING ACCOMPLISHED AT SLC IAW RED TABS. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 11OCT03, FACT 03OCT03 07:58 EWR R . REMOVED AND REPLAOct 2, 2003 · N374FE · Doug DC1010 · Door Warning SystemSDR 2000ZZZX654Web · crackedDURING MAINTENANCE, THREE 10 INCH CRACKS WERE FOUND ON RIGHT/CENTER WHEELWELL (Y=1386, Z=52) COMMON TO KEEL WEB, WEB DOUBLER, AND UPER WEB SPLICE, P/N'S, AEA0161-3, AEA0161-153, AND AEA0501 RESPECTIVELY. DATA WAS SENT TO BOEING/DOUGLAS 5-14-99 AND RESENT 7-9Feb 11, 2000 · N374FE · Doug DC1010 · Fuselage Miscellaneous StructureSDR 99FDEA00269Web · crackedDUR A/C P-F CONV AT AERONAVALI, 3 10' CRACKS WERE FOUND AT Y=1386 COMMON TO KEEL WEB, WEB DOUBLER & AEA0501 KEEL WEB UPPER SPLICE. REPAIRED KEEL WEB AND WEB DOUBLER PER IAW FEDEX EA NR 8-5314-44061.May 3, 1999 · N374FE · Doug DC1010 · Fuselage Main, KeelSDR 99FDEA00270Skin · crackedDUR A/C P-F CONV FOUND DAMAGE AT XIFH=288.14 ON THE UPPER SURFACE OF LT I/B FLAP SKIN. REMOVED AND REPLACED O/B UPPER SKIN SECTION DAMAGE ARC2369. SRM 57-10-00 FIG 4 IAW FEDEX IAW EA NR 8-5752-44069.Nov 27, 1998 · N374FE · Doug DC1010 · Wing, Plate/SkinSDR 99FDEA00271Bolt · corrodedDUR A/C P-F CONV CORROSION WAS FOUND IN ALL FOUR HOLE BORES COMMON TO ABA7003-2 & ABA7172 FITTINGS. THREE BOLTS FAILED IN TENSION. REMOVED AND REPLACED BOLTS FROM BORES IAW FEDEX EA NR 8-5311-41885.Oct 26, 1998 · N374FE · Doug DC1010 · Fuselage, Equipment Attach FittingsSDR 99FDEA00272Skin · corrodedDUR A/C P-F CONV ON EXT LWR FUSELAGE FROM BS 1099 TO BS 1541 CORROSION. REMOVED AND REPLACED FUSELAGE BELLY SKIN FROM Y=1119 TO Y-1308, BETWEEN L48L-L48R. REPAIRED THEN INSTALLED AN EXT SKIN SPLICE SIMILAR TO SRM 5320, FIG 17 AT Y-1308 TO RESTORE STRENGTH IAOct 2, 1998 · N374FE · Doug DC1010 · Fuselage Main, Plate/Skin
Back to N374FE, cancelled Mar 22, 2017