Pratt & Whitney JT9D-7A

Service difficulty reports · 593

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'JT9D7A'
  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 UPS04443337Bulb · inoperativeMAIN CARGO DECK CEILING EMERGENCY LIGHT FWD OF L1 DOOR HAS ONE BULB INOPERATIVE AND VERY DIM. REMOVED AND REPLACED MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST FWD OF L1 DOOR IAW MM 33-51-07. OPS CKS NORMAL.Oct 12, 2004 · N675UP · Boeing 747123 · Emergency LightingSDR P5CA0401245Panel · crackedRIGHT WING I/B FIXED T/E LWR PNL, I/B EXTENDED CHORD HAS CRACK 2 INCHES LONG AT WS 440. REMOVE CHORD INSTALLED NEW CHORD AS PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401246Frame · crackedMAIN DECK CEILING AREA FRAME WEB STA 960 STR 5R CRACKED. STOP DRILL CRACK PER SRM 51-30-02, 53-10-04, 51-00-00.Oct 11, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401247Stringer · crackedFUSELAGE STRINGER AT 10R HAS CRACK B/W STA 1372-1392. REMOVED DAMAGE AREA, REPLACED WITH NEW STRINGER AS PER SRM 53-10-03.Oct 11, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR P5CA0401248Skin · delaminatedRIGHT I/B ELEVATOR LWR SURFACE SKIN HAS DELAMINATION. REMOVED DAMAGE AREA, INSTALLED NEW PER SRM 51-40-04.Oct 11, 2004 · N858FT · Boeing 747123 · Elevator, Plate/SkinSDR P5CA0401249Frame · crackedAFT CARGO COMPT SECONDARY FRAME B/W STA 1740 & 1760 LBL 30 IS CRACKED. REMOVED DAMAGE FRAME & INSTALLED NEW FRAME PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401250Attach Fitting · crackedRIGHT WING L/E AFT ATTACHED FRAME (FSSI) TO WING FRONT SPAR UPPER CHORD HAS CRACKED AFT FSSI 335. REMOVED CRACK T-ANGLE & INSTALLED NEW T-ANGLE PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123 · Wing, Attach FittingsSDR P5CA0401236Floorbeam · crackedBULK CARGO COMPT FLOORBEAM LBL 38 STA 1980 IS CRACKED. REMOVED DAMAGE AREA, REPAIRED ANGLE, PRIMED & TREATED PER SRM 51-40-03.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Main, Floor BeamSDR P5CA0401240Rib · crackedRT HORIZONTAL STAB O/B RIB ASSY AT STAB BL 421.50 IS CRACKED. REMOVED CRACK AREA, NO FURTHER DEFECT FOUND. TREATED & PRIMED PER SRM 55-10-01 & 51-10-02.Oct 1, 2004 · N858FT · Boeing 747123 · Horizontal Stabilizer, Spar/RibSDR P5CA0401235Floor Support · crackedBULK CARGO COMPT FLOOR LONGITUDINAL BEAM AT STA 1960-2080 AT LBL 38 IS CRACKED. REMOVED DAMAGE AREA, INSTALLED NEW PARTS PER SRM 51-40-03, TREATED & PRIMED.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA0401237Spar · corrodedLT WING REAR SPAR LWR FIXED T/E PANEL I/B LWR BEAM AT WBL 128 HAS CORROSION AT FWD TENSION TRES. REMOVE CORRODED DOUBLER, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 51-40-02.Oct 1, 2004 · N858FT · Boeing 747123 · Wing SparSDR P5CA0401231Skin · delaminatedRT WING L/E UPPER SKIN BETWEEN WING STATIONS 445-476 LOWER SURFACE IS DELAMINATED. REMOVED PANEL & SENT TO COMPOSITE SHOP, REPAIRED & REINSTALLED PER SRM 51-40-09.Oct 1, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401233Skin · crackedAPU EXHAUST AREA SKIN CRACKED BS 2742. CUT OUT DAMAGED AREA, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 53-30-03.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Main, Plate/SkinSDR P5CA0401232Frame · crackedMAIN DECK CARGO COMPT SUPPORT FRAME AT STRINGER 10R, BODY STATION 1660, RBL 28 IS CRACKED. REMOVE FRAME, INSTALLED NEW SUPPORT FRAME, TREATED & PRIMED PER SRM 51-30-01 & 51-30-02.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401234Floorbeam · crackedBULK CARGO COMPT FLOORBEAM LBL 30 STA 1980 & 2000 IS CRACKED. REMOVED DAMAGE AREA, REPAIR ANGLE, TREATED & PRIMED PER SRM 51-40-03.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Main, Floor BeamSDR P5CA0401238Skin · corrodedRT HORIZONTAL STAB T/E UPPER SURFACE ENTIRE LENGTH SKIN SEVERAL AREA HAS CORROSION. REMOVE CORROSION FROM SEVERAL AREAS, TREATED & PRIMED PER SRM 51-10-01, 55-10-01, 51-10-02.Oct 1, 2004 · N858FT · Boeing 747123 · Horizontal Stabilizer, Plate/SkinSDR UPS04443328Plate · crackedINSPECTION TYPE-C, CRACK FOUND AT BS 1241 WL 200 RT SPLICE PLATE NR 5 BOLT HOLES BORE CRACK STILL REVEALED AFTER THE HOLE OVERSIZED TO DIA 1.200 INCH. RT SPLICE PLATE REPLACED IAW EO B747-5740-4366.Oct 1, 2004 · N681UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS04443321Splice · crackedINSPECTION TYPE-C, LT WING UPPER BS 1241 WL 180 REAR SPAR SPLICE PLATE FASTENER HOLE NR 7 FOUND CRACKED AT SPAR CHORD UPPER LAYER RUNNING AFT APPROX .0625 INCH LONG. HOLE REWORKED AND OVERSIZED IAW EO B747-5740-17032.Sep 30, 2004 · N681UP · Boeing 747121 · Wing Main, Frame StructureSDR P5CA0401227Skin · damagedPRIOR TO DEPARTURE FOUND DAMAGE ON FWD CARGO DOOR LWR SKIN. REPAIRED DAMAGE AT LWR CORNER SKIN PER SRM 52-30-06, FIGURE 1 SHEET 7.Sep 27, 2004 · N920FT · Boeing 747249F · Cargo/Baggage DoorsSDR UPS04443271Stringer · corrodedINSPECTION TYPE-C FWD CARGO STA 860-880 S47L STRINGER CORROSION FOUND. FWD CARGO BS 860-880 STR 47L STRINGER REPAIRED IAW SRM 53-10-03 FIG 1 DUE TO BLEND OUT DEPTH 0.040 INCH , WIDTH 1 INCH AND LENGTH 2 INCHES OUT OF SRM 53-10-01 FIG LIMITATION.Sep 26, 2004 · N681UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS04443391Link · corrodedINSPECTION TYPE-C FX- KEEL BEAM BOX INNER HORIZ SUPPORT LINK CORRODED AT BS 1460 WL 118. CORROSION MACHINED OFF AT BOTH SIDE VERTICAL RIBS 0.030 INCH AT BOTTOM HORIZ RIB 0.020 INCH . KEEL BEAM BOX INNER HORIZ SUPPORT LINK REPLACED IAW HX RS NR R-53-49-35206Sep 25, 2004 · N681UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS04443350Gate · crackedINSPECTION TYPE-C M/D- R5 DOOR UPR GATE CRACKED. (BS 2240 TO 2280, STR R16 TO R17) UPPER GATE REPLACED IAW MM 20-51-01.Sep 24, 2004 · N681UP · Boeing 747121 · Service DoorsSDR UPS04443377Rib · crackedINSPECTION TYPE-C, RT WING L/E OLES 1453 NR25 VC FLAP OB ROTARY IB SUPPORT RIB FWD MOUNT HOLE CRACKED. RT WING L/E OLES NR25 VC FLAP OB ROTARY ACTUATOR IB SUPPORT RIB REPAIRED IAW HX RSNR R-57-41-35205, DVI THE AFFECTED AREA AT C- CHECK INTERVALS NOT TO EXCESep 23, 2004 · N681UP · Boeing 747121 · Wing, Rib/BulkheadSDR P5CA0401194Stringer · corrodedAFT CARGO COMPT STRINGER 51R HAS CORROSION. REMOVED LITE CORROSION MATERIAL, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR P5CA0401195Floorbeam · crackedBULK CARGO COMPT FLOORBEAM CRACKED. REMOVED & REPLACED DAMAGED AREA.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Floor BeamSDR P5CA0401196Skin · corrodedRIGHT UPPER WING SKIN HAS CORROSION ALONG FWD OF MID SPAR. BLENDED OUT CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401197Floor Support · crackedBULK CARGO COMPT LONGITUDINAL FLOOR SUPPORT CRACKED. REMOVED AND REPLACED DAMAGE AREA.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA0401198Bulkhead · corrodedAFT BULKHEAD UNDER FLOOR & WEB CORRODED. REMOVED STIFFENER & WEB FROM FLOORBEAM, INSTALLED NEW ONE.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, BulkheadSDR P5CA0401199Skin · corrodedAFT FUSELAGE HAS SKIN CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Plate/SkinSDR P5CA0401200Skin · corrodedLEFT WING UPPER SKIN 24 INCHES FWD OF SPAN WISE BEAM NR 2 HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA0401201Frame · corrodedCENTER CARGO COMPT FRAME UPPER CHORD HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA0401202Seat Track · corrodedCABIN LEFT SEAT TRACK HAS CORROSION SPOTS. REMOVED CORROSION .020 MATERIAL WITHIN LIMITS.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0401203Frame · corrodedBULK CARGO COMPT FUSELAGE FRAME, UPPER CHORD TOP & BOTTOM HAS SURFACE CORROSION. REMOVE CORROSION, ORIGINAL MATERIAL IS 0.085, AFTER REWORK 0.083 WITHIN LIMITS.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401204Seat Track · corrodedMAIN DECK CARGO COMPT SEAT TRACK HAS CORROSION. REMOVED CORROSION, PRIMED & TREATED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0401206Keelbeam · corrodedKEEL BEAM APPROX STA 1093 HAS BOTTOM SURFACE CORROSION. REMOVED CORROSION, AFTER WORK IT IS 0.061, OK PER SRM 52-10-01.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, KeelSDR P5CA0401208Skin · corrodedLT WING MID FLAP ENTIRE CENTER SECTION PANEL HAS SEVERAL CORROSION SPOTS. REMOVED SURFACE CORROSION , PRIMED AND TREATED.Sep 14, 2004 · N858FT · Boeing 747123 · Trailing Edge FlapsSDR P5CA0401207Web · crackedFWD CARGO COMPARTMENT WEB CRACKED. REMOVED CRACKED WEB, FABRICATED NEW WEB AND INSTALLED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA0401209Floor Panel · corrodedFWD CARGO FLOOR PANEL HAS CORROSION. REMOVED SURFACE CORROSION, TREATED AND PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Floor PanelSDR P5CA0401215Keelbeam · corrodedKEEL BEAM BOX BOTTOM SURFACE HAS CORROSION LEFT & RIGHT SIDE. REMOVED FASTENER, REMOVED CORROSION & REINSTALLED FASTENER, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, KeelSDR P5CA0401205Fairing · delaminatedWING TO BODY FAIRING 1916L HAS DELAMINATION. CLEANED AREA & REBONDED.Sep 14, 2004 · N858FT · Boeing 747123 · Aerodynamic FairingsSDR P5CA0401217Keelbeam · corrodedKEEL BEAM BOX, PANEL SUPPORT STRUCTURE INNER LIP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, KeelSDR P5CA0401226Frame · corrodedCTR CARGO COMPT FRAME TOP OF UPPER CHORD AT STA 1740 RBL 40 IS CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALLED NEW CHORD.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401219Floor Panel · crackedBULK CARGO LEFT SIDE FLOOR PANEL BS 2040-2160 DENTED & CRACKED. CUT OUT DAMAGE AREA, FABRICATED & INSTALLED DOUBLER, PRIME & TREATED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Floor PanelSDR P5CA0401216Fitting · corrodedLEFT NOSE WELL BULKHEAD O/B SIDE OF NLG LWR STR FITTING IS CORRODED. REMOVED CORROSION, PRIMED & TREATED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA041224Skin · corrodedEXTERNAL SKIN AT STA 255 STR 32L AT LAP JOINT DELAMINATION. REMOVED BULGE, NO CORROSION FOUND, REMOVED FASTENER, INSTALLED NEW FASTENER, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Plate/SkinSDR P5CA0401218Skin · corrodedFWD CARGO DOOR/LWR AFT SKIN HAS CORROSION. REMOVED CORROSION, FABRICATED DOUBLER & FILLER.Sep 14, 2004 · N858FT · Boeing 747123 · Cargo/Baggage DoorsSDR P5CA0401211Skin · corrodedFUSELAGE SKIN JOINT HAS SURFACE CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Plate/SkinSDR P5CA0401213Seat Track · corrodedLEFT CENTER SEAT TRACK DIRTY & CORRODED. REMOVED MINOR CORROSION FROM TRACK, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0401223Panel · crackedAFT CARGO COMPT WALKWAY PANEL STA 1775-1795 LBL 22-45 HAS CRACKS, & CORROSION. REMOVED CORROSION, BLENDED & CUTOUT CRACK, FABRICATED DOUBLER, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Floor PanelSDR P5CA0401225Skin · crackedLEFT WING UPPER SURFACE O/B NR 2 PYLON L/E AREA 3 PLACES OF CRACKED SKIN. REMOVED SPLICE PLATE CRACK, FABRICATED SPLICE PLATE, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Nacelle/Pylon, Plate/Skin
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