N995FD

Service difficulty reports · 111

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 = 'N995FD' 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 FDEA201204021220Guard · out of adjustTHE EMERGENCY LIGHTS GUARD CANNOT BE CLOSED WITH THE SWITCH IN ARM, WITHOUT THROWING THE SWITCH TO OFF. RESET SAFETY GUARD ON EMERGENCY LIGHT SWITCH. SYS OPS CHECKED GOOD IAW AMM 33-51-00-5-0.Apr 2, 2012 · N995FD · Boeing 7572Q8 · Emergency LightingSDR FDEA201111285065Skin · misrepairedSKIN AT BS 530, S26-27R MISREPAIRED. REPAIRED IAW EAF-5330-152662.Nov 28, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201111174970Door Frame · corrodedMAIN CARGO DOOR FRAME AT BS 1645 HAS CORROSION ON LOWER END WL 210 INBD FLANGE, LT SIDE, LBL 55. REMOVED CORROSION IAW SRM-51-10-02, CHECKED LIMITS: ORIGINAL MATERIAL .063, AFTER RE-WORK .046, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07, PG 108 FIG 101, DETAINov 17, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201111174969Frame · corrodedFRAME AT STA 1645 LOWER END HAS CORROSION AT W.L.210, INBD FLANGE RBL 55. REMOVED CORROSION IAW-SRM-51-10-02, ORIGINAL MATERIAL .063 AFTER REWORK .055, REMOVED .008 FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07, PG 103, FIG 101, DETAIL II. REPAIR WAS ACCOMPLISHENov 17, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201111044752Frame · misrepairedAFT CARGO, BS 1220 FRAME S24R-S26R, MISREPAIRED. REMOVED FRAME IAW SRM 51-40-02. REPLACED FRAME IAW SRM 51-40-02, AND DWG 146N1027. MAJOR REPAIR.Nov 4, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201110284679Skin · unknownSKIN MISREPAIRED AT BS 1630, S24-26L. REPAIRED IAW EA F-5330-152661.Oct 28, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201110194580Stringer · noneEXISTING STRINGER REPAIR AT STA 1573, STR 27R, REQUIRES SUPPLEMENTAL INSP. PERFORM THE SUPPLEMENTAL INSP ON THE STRINGER REPAIR AREA IAW THE SRM 53-00-03, FIG 201, REPAIR 1, TABLE IV, ZONE 1 REQUIREMENTS IAW FORM 8100-9, DATED OCT 17, 2011. REF: N00121 FOR SKIOct 19, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201110184569Skin · damagedSKIN DAMAGED AT BS 1604-1620, STR 18-21R. REPAIRED IAW EA 757-5361-F3555.Oct 18, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201110144498Gate · corrodedPASSENGER R1 DOOR LOWER GATE BOTTOM EDGES HAS GOUGED AND CORROSION. R & R LOWER GATE IAW AMM 52-11-38-4. REMOVED CORROSION ON GATE IAW SRM 51-10-02 CHECKED LIMITS IAW SRM 52-10-02 ORIG MAT 170 MAT REMAINING AFTER BLEND .040. FOUND TO BE OUT OF LIMITS IAW SOct 14, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201110104411Skin · misrepairedSKIN AT BS 1540-1580, S2-3L MISREPAIRED. REPAIRED IAW EA F-5330-147745.Oct 10, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201110104412Gate · corrodedR-4 DOOR LOWER GATE HAS CORROSION AROUND THE SEAL RETAINER BRACKET. REMOVED CORROSION FROM R-4 DOOR LOWER GATE FOUND TO BE OUT OF LIMITS I.A.W. SRM 52-10-02 FIG 101. REMOVED AND REPLACED LOWER GATE ASSY IAW MM 52-11-38. PERFORMED R-4 DOOR ADJUSTMENT IAW MOct 10, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201110064351Strap · corrodedLT HORIZONTAL STAB PIVOT FITTING UPPER STRAP HAS CORROSION. ACCOMPLISHED EA F-5510-152652. CORROSION WAS DETERMINED TO BE OUT OF LIMITS PER SRM 55-10-01, PAGE 104, FIG.101, DETAIL 3.Oct 6, 2011 · N995FD · Boeing 7572Q8 · Horizontal Stabilizer StructureSDR FDEA201110044286Seat Track · corrodedSEAT TRACK CORRODED AT BS 1280, RBL 24. REMOVED CORROSION WITH .013" MATERIAL LOSS, WITH .072" REMAINING, ORIGINAL WAS .085". FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. FABRICATED NEW SEAT TRACK FROM BAC 1520-792, BATCH 1964663. LOCATED AND DRILLOct 4, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109294209Gate · corrodedL-1 DOOR LOWER GATE HAS PITTED CORROSION AROUND THE SEAL RETAINER BRACKET. REMOVED AND REPLACED LOWER GATE ASSY, PER AMM 52-11-38. PERFORMED DOOR ADJUSTMENT CHECKED PER AMM 52-11-00-5 CHECKED GOOD, MAJOR REPAIR.Sep 29, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201109294210Firewall · chafedNR 2 PYLON INBD SIDE FWD FIREWALL AFT SIDE CHAFED. REPAIRED IAW EA F-5450-147735. MAJOR REPAIR.Sep 29, 2011 · N995FD · Boeing 7572Q8 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201109294208Skin · crackedLT WING L/E GAP PANEL,114N1801-951, ABOVE PYLON HAS APROX 1' CRACK IN SKIN. REMOVED SKIN FROM LT WING GAP PANEL IAW SRM 51-40-02, FABRICATED NEW SKIN ON TR T11/896272, LOCATED & DRILLED IAW SRM 51-40-05, INSTALLED NEW SKIN, 5 EA FITTINGS AND PANEL IAW SRM 5Sep 29, 2011 · N995FD · Boeing 7572Q8 · Wing, Plate/SkinSDR FDEA201109244115Skin · misrepairedSKIN AT STA 1480 S26L- S28L MISREPAIRED. REPAIRED IAW SRM 51-40-02 & 53-00-01, TABLE I & II, FIG 201 P203 REPAIR 16. CATEGORY B MAJOR REPAIR.Sep 24, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201109244114Gusset · chafedNR2 PYLON OTBD AFT LOWER CORNER CHAFED. COMPLIED WITH EA F-5450-147737. MAJOR REPAIR.Sep 24, 2011 · N995FD · Boeing 7572Q8 · Nacelle/Pylon, Main FrameSDR FDEA201109224068Gate · corrodedR2 DOOR LOWER GATE CORRODED. R & R R2 DOOR LWR GATE ASSY, IAW AMM 52-11-38 AND ADJUSTED R2 DOOR IAW AMM 52-11-00-5 CHECKED GOOD. REMOVAL OF CORROSION WAS FOUND TO BE OUT LIMITS IAW SRM 52-10-02, FIG 101, DETAIL 5. MAJOR REPAIR.Sep 22, 2011 · N995FD · Boeing 7572Q8 · Service DoorsSDR FDEA201109193966Stringer Splice · crackedAFT CARGO STA 1620 AT S-25R SPLICE IS DENTED. R & R 5 EA FASTENERS F.O.M IAW SRM 51-40-02. FOUND SPLICE TO BE CRACKED AND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, SH 1, P.101. RECEIVED SPLICE ON MAE TRAVELER T11/894584, PN FX-146N3820-56. REMOVED CRACKED SSep 19, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201109193968Skin · misrepairedSKIN MISREPAIRED AT STA 1701-1720 S16L-17L. REPAIRED IAW EA 757-5361-16-F3556.Sep 19, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201109163912Seat Track · gougedSEAT TRACK AT STA 418, STA 440, LBL 45 IS GOUGED. BLENDED GOUGE ORIGINAL: .200", AFTER: .140", LOSS: .060"; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. FABRICATED SEAT TRACK, BAC1520-792, BATCH NR 1904663, IAW SRM 53-10-52, FIG 1, DETAIL 3Sep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109163908Seat Track · gougedSEAT TRACK AT BS 418 - 440, LBL 24, IS GOUGED. BLENDED GOUGE AREA; ORIGINAL: .200", AFTER: .150", FOUND TO BE OUT OF LIMTS IAW SRM 53-00-52, FIG 101, DETAIL 1, REWORK AREA 2"X.9". R & R SEAT TRACK IAW SRM 51-40-02, REPLACEMENT SEAT TRACK, BATCH NR 00019046Sep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109163907Seat Track · gougedSEAT TRACK AT STA 418-STA 440 RBL 24 GOUGED. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02. TREATED AND PRIMED PER SRM 51-20-01. PAINTED PER SRM 51-20-01. INSTALLED NEW SEAT TRACK, PER SRM 51-40-0Sep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109163906Seat Track · gougedSEAT TRACKAT STA 418, STA 440, RBL 48 IS GOUGE. BLENDED GOUGE ORIGINAL MAT .200, AFTER REPAIR .130 MATERIAL, REMOVED .070, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I, FIG 101. R & R SEAT TRACK MATERIAL BAC1520-792, BATCH 1904663 IAW SRM 51-40-02, MASep 16, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109153895Skin · misrepairedSKIN AT BS 1681 S-17L -S-18L MISREPAIRED. R & R REPAIR IAW SRM 51-40-02, FABRICATED NEW REPAIR IAW SRM 53-00-01, TABLE I & III FIG 101, PG 203. MAJOR REPAIR.Sep 15, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201109133863Door Frame · gougedPASENGER DOOR 1 L FWD DOOR FRAME AT BS 337.5, ADJACENT TO S8L GOUGED. BLENDED GOUGE IAW 51-10-02 CHECKED LIMITS, ORIGINAL MAT .063" AFTER REWORKED .038" FOUND TO OUT LIMITS IAW SRM 53-10-15, FIG 101 DETAIL IV. REMOVED FRAME IAW SRM 51-40-02, FABRICATED, LOCASep 13, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201109103820Tee Fitting · corrodedMCD AFT PRESSURE DECK UPON REMOVAL FOUND TEE ANGLE CORRODED BS 1720 LBL-50 REMOVED TEE ANGLE FOR ACCESS TO CORROSION, PER SRM 51-40-02. REMOVED CORROSION PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-80-05, DETAIL 9, P.109. LOCATED AND DRILLED NEW TEESep 10, 2011 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201109103819Cusp Web · corrodedAFT PRESSURE DECK UPON REMOVAL OF DECK FOUND CUSP WEB CORRODED LBL-55, STA 1701-STA 1720.Sep 10, 2011 · N995FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201109103818Fitting · corrodedAFT PRESSURE DECK UPON REMOVAL, FOUND FITTING CORRODED.Sep 10, 2011 · N995FD · Boeing 757225 · Fuselage Main, Attach FittingsSDR FDEA201109093813Wedge · damagedRT WING INBD FLAP, TRAILING FLAP WEDGE HAS DAMAGE AT T/E 21 INCHES FROM OTBD EDGE. REPAIRED IAW SRM 51-70-10 REPAIR 4. MAJOR REPAIR.Sep 9, 2011 · N995FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201109063718Frame · damagedFWD CARGO DOOR FWD LOWER CORNER ANGLE FRAME DAMAGE. REPLACED LOWER CORNER ANGLE FRAME IAW SRM 51-40-02, CHECKED LIMITS MAT FOUND TO BE PUNCTURED THROUGH THE LOWER CORNER FRAME & EXCEED THE ALLOWABLE DAMAGE IAW SRM 52-30- 02, FIG 101 NOTE L=1.0" W=0.5" RECEISep 6, 2011 · N995FD · Boeing 7572Q8 · Cargo/Baggage DoorsSDR FDEA201109033645Skin · corrodedLWR FUSELAGE HAS CORROSION ON SKIN RUNNING UNDER RAIN DIVERTER FOR POTABLE WATER SERVICE AT BS 1661.Sep 3, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108313598Crease Beam · gougedCREASEBEAM AT BS 1290-1370 HAS NUMEROUSE GOUGES AND SCRATCHES. FUTHER INVESTIGATION FOUND A PUNCTURE HOLE WAS FOUND, IAW SRM 53-60-15, FIG 101, DETAIL IV. NOTE C, PUNTURE HOLES ARE NOT PERMITED ADJACENT TO FASTENER HOLES LESS THAN 1" AWAY, R & R DAMAGEAug 31, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201108253486Gate · corrodedL-2 DOOR LOWER GATE HAS PITTED CORROSION AT SEAL RETAINER BRACKET. REMOVED CORROSION, CHECKED LIMITS ORIG .200 REMOVED .035 REMAINING .165 FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101. REMOVED LOWER GATE ASSY IAW AMM 52-11-38. RECEIVED NEW GATE ASAug 25, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108243461Seat Track · misalignedSEAT TRACK, RBL 45, STA 440. DOES NOT JIG (MISALIGNED). SPLICED A NEW SEAT TRACK SECTION BETWEEN BS 440-490, RBL 45, IAW SRM 53-00-52, FIG 201. MAJOR REPAIR.Aug 24, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108133260Gate · corrodedL-4 DOOR LOWER GATE CORRODED AT SEAL RETAINER BRACKET. REMOVED CORROSION AT LOWER SEAL AREA . CHECKED LIMITS ON WORKED AREA FOUND OUT OF LIMITS IAW SRM 52-10-02, FIG 101. ORIG MAT .200 MAT LOSS .040 REM. 160. REMOVED L-4 LOWER GATE IAW 51-40-02. RECEIVEDAug 13, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108133259Skin · dentedDOOR OUTER SKIN HAS AN OUTER DENT AT S13R,4" FROM L/E. EVALUATED DENT ON R-1 DOOR OUTER SKIN AT S13R, 4" FROM THE L/E;W=.008", D=.007, A/Y=114. DENT IS W/I LIMITS IAW SRM 52-10-01, FIG.101, DETAIL7. HFEC IAW NTM 51-00-19,PT.6, NO CRACKS NOTED. APPLIED DENAug 13, 2011 · N995FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201108043099Floorbeam · corrodedFLOORBEAM AT LBL 45 CORRODED AT STA 377. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201, REPAIR NR 3 AT STA 377 FROM RBL 24 TO LBL 70. MAJOR REPAIR.Aug 4, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201108033088Pressure Deck · corrodedPRESSURE DECK WEB HAS CORROSION AT STA 1681.8-1720, RBL 50. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS MAT THICKNESS .071", BLENDED MAT, .053" FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DET III, REMOVED PRESSURE WEB IAW SRM 51-40-02. FABRICATED PRAug 3, 2011 · N995FD · Boeing 7572Q8 · Fuselage Floor PanelSDR FDEA201108023316Skin · gougedAPU DOOR 316AR EXTERNAL SKIN LATCH HOLES, -2- PLACES GOUGED WITH KNIFE EDGE.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Auxiliary Power Unit (APU) DoorsSDR FDEA201108023430Seat Track · misalignedSEAT TRACK, LBL 45, BS 440 MISALIGNED. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW DWG 143N5110, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05 AND DWG 143N5110 INSTALLED SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5110 AND PART MARKEDAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201108023142Stringer · corrodedDURING A CHECK, INSTALLED DOUBLER REPAIR AT STA.1500, STR 22L,FOUND S-22L CORRODED AROUND FASTENER HOLES AT STA 1510. CUT OUT DAMAGED STRINGER 22L BTW BS 1510 TO BS 1530 IAW SRM 53-00-03 REPAIR 2 PG 201, RECEIVED FABRICATED STRINGER, FABRICATED SPLICE Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201108023431Skin · dentedSKIN DENTED AT BS 1540, S-23-24R. REMOVED DAMAGE & FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, DETAIL 3, FIG. 101 & SRM 51-40-02. HFEC , NO CRACK INDICATION NOTED. FABRICATED DOUBLER PER SRM 53-00-01, TABLE 1 / 3, FIG. 201, REPAIR 16. INSTALLED DOUBLER PAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023314Seat Track · gougedSEAT TRACK GOUGE AT STA 1210 TO 1220, LBL 45 AROUND THE CROWN AREA. REMOVED ANGLE AND SEAT TRACK IAW SRM 51-40-02, FABED NEW PART IAW SRM 53-00-52, FIG 201 SHEET 1, BATCH 1904663, PN BAC 1520-792, LOCATED AND DRILLED IAW SRM 51-40-05, TREATED AND PRIMED ANAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023364Seat Track · misinstalledSEAT TRACK STA 440, RBL 24, DOES NOT JIG. CUT OUT SECTION OF SEAT TRACK AT BS 440-470 IAW SRM 53-00-52, REPAIR 1. FABRICATED NEW SEAT TRACK AND REPLACED IAW SRM 53-00-52, FIG 201 REPAIR 1. MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023322Seat Track · misalignedSEAT TRACK, STA 440-470, LBL 24, DOES NOT JIG. CUT OUT SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, FIG 201, SHEET 1 OF 5, REPAIR 1. MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108023278Skin · misrepairedSKIN AT 1560-1580, S-18R-S19R DOES NOT MEET SRM REPAIR STANDARDS. CORRECTED REPAIR IAW SRM 53-00-01. MAJOR REPAIR.Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023096Skin · misrepairedFUSELAGE SKIN REPAIR AT BS 343-346, S-21R-S-23R IS NOT IN COMPLINCE WITH SRM. REMOVED EXISTING REPAIR AT BS 343-346 S-21R - S-23R IAW SRM 51-40-02 , HFEC INSP IAW NTM 51-00019 PT6 & 51-00-16 PT6, FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 53-00-01 REPAIR Aug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201108023101Skin · misrepairedSKIN AT BS 1380-1400, S-23L-S-25L MISREPAIRED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-02 AND SRM 53-00-01, REPAIR 16. FABRICATED DOUBLER PER SRM 53-00-01, TABLE 1 AND 2, FIG. 201, P. 203. MAJOR REPAIRAug 2, 2011 · N995FD · Boeing 7572Q8 · Fuselage Main, Plate/Skin
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