Boeing 757-2T7

Service difficulty reports · 666

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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 aircraft_model_key = '7572T7'
  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 FDEA201005051467Transition Panel · corrodedFWD CARGO COMPT RT TRANSITION SIDE PANEL AT STA 645.75-765.75 FOUND CORRODED. CORRODED SIDE TRANSITION PANEL FROM STA 645 TO STA 765 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.May 5, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201005051455Floor Support · corrodedCABIN : FLOOR SUPPORT AT STA 362, LBL 60 HAS EXFOLIATION CORROSION. CORRODED SUPPORT AT STA 362, LBL 60 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.May 5, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201005041439Fitting · corrodedFWD CARGO COMPARTMENT RH CARGO NET TIE-DOWN FITTINGS AT STA 620, STA 640 AND STA 660 FOUND WITH CORROSION. TIE DOWN FITTING FOUND DEEP PITTING CORROSION EXCEEDED LIMIT AS PER SRM 53-00-53 FIG. 101 REV, 99. CORRODED PLATE AT STA 620 RT R & R WITH NEW PLATE May 4, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201005041442Intercostal · corrodedTOP OF INTERCOSTAL HAS CORROSION AT STA 324 TO STA 345, LBL 20". CORRODED INTERCOSTAL FROM STA 324 TO STA 345 REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201005041441Seat Track · corrodedCABIN FUSELAGE INTERIOR LT SEAT TRACK WITH CORROSION AT LT BS 680 TO BS 740, LBL 45.5. CORRODED SEAT TRACK FROM LT BS 680 TO BS 740. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005041434Transition Panel · corrodedAFT CARGO COMPT RT TRANSITION SIDE PANEL AT STA 1530-1640 FOUND CORRODED. CORRODED TRANSITION PANEL FROM STA 1530 TO STA 1640 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201005021428Frame · unknownCABIN FUSELAGE INTERIOR FRAME WITH EXISTING REPAIR DOUBLER AT STA 1140, BETWEEN STRINGER S-1L TO S-3L. CABIN MAIN FRAME AT STA 1140, S-6L TO S-6R REPAIRED IAW SRM 53-00-07 REPAIR 1, REV. 99. INITIAL INSP THRESHOLD AT 50,000 FLIGHT CYCLES AND AN INTERVAL INSPMay 2, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, FrameSDR FDEA201005021427Frame · unknownCABIN FUSELAGE INTERIOR FRAME WITH EXISTING REPAIR DOUBLER AT STA 1120, BETWEEN STRINGERS S-1L TO S-3L. CABIN MAIN FRAME AT STA 1120, S-7L TO S-4R REPAIRED IAW SRM 53-00-07 REPAIR 1, REV. 99. INITIAL INSPECTION THRESHOLD AT 50,000 FLIGHT CYCLSES AND AN INTMay 2, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, FrameSDR FDEA201005021426Transition Panel · corrodedAFT CARGO COMPT LT TRANSITION PANEL AT STA 1530-1640 FOUND CORRODED. CORRODED TRANSITION PANEL FROM STA 1530 TO STA 1640 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFED AS MINOR IAW GMM 6-2-100.May 2, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281389Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1540, STA 1580, STA 1600 AND STA 1620 FOUND WITH CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.022" AT STA 1540 LT, STApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281388Fitting · corrodedFWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 520, STA 540 AND STA 560 FOUND WITH CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.025" AT STA 520 LT, 0.035" AT STA 540 Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281387Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1300, STA 1320, STA 1360 AND STA 1380 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.021" STA 1300, STA 1320, STA 1340 AND STA 1360 RT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIMIT IAW E.A.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281386Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1540, STA 1560, STA 1580 AND STA 1600 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.021" AT STA 1540, STA 1560, STA 1580 AND STA 1600 RT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIMIT IAW Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281385Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1400, STA 1420, STA 1480, STA 1500 AND STA 1520 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIALS REMOVED 0.025" AND STA 1400, STA 1420, STA 1480, STA 1500, AND STA 1520 LT, MATERIAL REMAINED 0.155, Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004281384Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 1220, STA 1240, STA 1260 AND STA 1260 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.030" AT STA 1220 RT, STA 1240 RT, STA 1260 RT AND STA 1280 RT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281383Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1220, STA 1240, STA 1260 AND STA 1300 FOUND WITH CORROSION. FITTING RE-WORKED AREA MATERIAL REMOVED 0.022" AT STA 1220, STA 1240, STA 1260 AND STA 1300 LT ORIGINAL THICKNESS 0.180" FOUND WITHIN LIMIT IAW EApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281381Fitting · corrodedFWD CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 760, STA 780 AND STA 840. FOUND WITH CORROSION. REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.036" AT STA 760 RT, 0.025" AT STA 780 RT ANApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004281380Fitting · corrodedFWD CARGO COMPT, RT CARGO NET TIE-DOWN FITTINGS AT STA 680, STA 720 AND STA 740 FOUND WITH CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.022" AT STA 680 RT, 0.032" AT STA 720Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281379Fitting · corrodedAFT CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT BS 1460, 1480 AND 1500 FOUND WITH CORROSION. REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. TIE DOWN FITTING RE-WORKED AREA MATERIAL REMOVED 0.020" AT STA 1460, STA 1480, STA 1500 AND STA 1520 RApr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004281378Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS STA 1320, STA 1360 AND STA 1380. (QTY2) FOUND WITH CORROSION. TIE DOWN FITTING FOUND DEEPLY CORRODED EXCEEDED LIMIT AS PER SRM 53-0053 FIG. 101, REV. 99. CORRODED PLATE AT STA 1380 R & R WITH NEW PLAT 451N5700-8Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004281374Transition Panel · corrodedAFT CARGO COMPT RT TRANSITION SIDE PANEL UNDER SURFACE AT STA 1440 FOUND WITH CORROSION. CORRODED TRANSITION PANEL AT STA 1440 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281373Panel · corrodedAFT CARGO COMPT LT TRANSITION SIDE PANEL AT STA 1445-1530 FOUND CORRODED. PANEL R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281372Panel · corrodedAFT CARGO COMPT RT TRANSITION SIDE PANEL AT STA 1440-1530 FOUND CORRODED. PANEL R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281371Panel · corrodedAFT CARGO COMPARTMENT RT TRANSITION SIDE PANEL AT STA 1310-1380 FOUND CORRODED. PANEL R & R IAW SRM 51-40- 02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281370Support · crackedNLG WHEEL WELL LT SEAL RETAINER SUPPORT PLATE AT STA 390 CRACKED. CRACKED RETAINER SUPPORT PLATE AT STA 390 R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004281369Panel · corrodedAFT CARGO COMPARTMENT LT TRANSITION SIDE PANEL AT STA 1200-1300 CORRODED. CORRODED TRANSITION PANEL BETWEEN STA 1200 AND STA 1310, R & R IAW SRM 51-40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100.Apr 28, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004271366Fitting · corrodedFWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 580, ST 660 AND STA 720 FOUND WITH CORROSION. FWD CARGO BS LT CARGO NET TIE-DOWN FITTINGS AT BS 580, 660 & 720. FOUND CORRODED. REMOVED & TREATED IAW SRM 51-10-02 AND 51-20-01 REV 99. MATERIAL REMOVEDApr 27, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Attach FittingsSDR FDEA201004211263Panel · corrodedAFT CARGO COMPARTMENT LT TRANSITION PANEL AT STA 1200-1310 FOUND CORRODED. CORRODED AFT CARGO COMPARTMENT TRANSITION PANEL FROM LT STA 1200 TO STA 1310. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 21, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004211262Frame · corrodedFWD LT WING-TO-BODY FAIRING ATTACH FRAME WITH LIGHT CORROSION AT BS 860 TO BS 900, LBL 7. CORRODED FRAME FROM BS 860 TO BS 900 AT LBL 7. R & R IAW SRM 51- 40-02 REV. 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 21, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004201256Skin · corrodedAFT RT CREASE BEAM PANEL UPPER SKIN SURFACE CORROSION ADJACENT TO CORNER FITTING AT BS 1720, RBL 45.50. CORRODED BEAM PANEL AT BS 1720 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 20, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Plate/SkinSDR FDEA201004191253Floorbeam · corrodedCABIN AFT FLOORBEAM WITH CORROSION AT UPPER CHORD SURFACE AND SURROUNDING FASTENER HOLES AREA AT BS 1661, BETWEEN RBL 58 AND LBL 58. CORRODED BEAM AT BS 1661 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201004191223Floor Support · corrodedCABIN AFT FLOOR INTERCOSTAL UPPER CAP WITH CORROSION AT FASTENER HOLES AREA BETWEEN BS 1661 AND BS 1681, AT RBL 0. R & R AS PER SRM 51-40-02, REV 99. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004191222Floor Support · corrodedCABIN AFT FLOOR INTERCOSTAL WEB UPPER CAP WITH CORROSION AT FASTENER HOLES AREA BETWEEN BS 1661 TO BS 1681, AT RBL9. R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR FDEA201004191221Floor Skin · corrodedCABIN AFT LT DECK PLATE UPPER SURFACE WITH CORROSION AT BS 1681 TO BS 1720, BETWEEN BL0 AND LBL 58. CORRODED DECK PLATE FROM BS 1681 TO BS 1720 R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 19, 2010 · N937FD · Boeing 7572T7 · Fuselage Floor PanelSDR FDEA201004151200Panel · corrodedNR 1 ENGINE NACELLE STRUT ACCESS PANEL NR 433GR CUTOUT AREA AT STA 120, INTERNAL SURFACE CORROSION. CORRODED PANEL NR 433GR R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 15, 2010 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/SkinSDR FDEA201004081099Floorbeam · corrodedTOP OF FLOORBEAM HAS CORROSION AT STA 377, BL 0 TO LBL 22. FLOORBEAM AT STA 377, LBL 62 TO RBL 62 FABRICATED IAW DWG 141N5123, SHEET 1, REV 1, IAW GMM 7-0-1001 REV. 110. FLOORBEAM R & R IAW SRM 51-40-02 REV 99. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-Apr 8, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201004081098Floorbeam · corrodedFUSELAGE INTERIOR CABIN AFT FLOORBEAM WITH CORROSION AT UPPER CHORD SURFACE AND SURROUNDING FASTENER HOLES AREA AT BS 1640, BETWEEN RBL 24.75 AND LBL 24.75. CORRODED FLOORBEAM R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Apr 8, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201004051059Panel · crackedWING L/E SLAT NR2 AFT INBD PANEL HAS A CRACK WITH STOP HOLE. CRACK STARTS FROM L/B MAIN TRACK ATTACHMENT AREA. ADJUSTMENT AND OPS TEST OF THE NR 2 L/E SLAT AFTER INSTALLATION CARRIED OUT AND FOUND GOOD IAW AMM 27-81-02, REV 5.2. THIS REPAIR IS CLASSIFIED ASApr 5, 2010 · N937FD · Boeing 7572T7 · Leading Edge DevicesSDR FDEA201003301035Frame · damagedINTERIOR FRAME WITH DOUBLE HOLE AND CLOSE SPACED HOLES AT BS 418, BETWEEN STR 2L TO STR 2R. FRAME AT BS 418, STR 2L TO STR 2R, REPAIRED IAW STA EA 757-5312-08-E0612 (EXTRANEOUS FASTENER HOLES FOUND ON STA 395 AND STA 418 FRAMES, BETWEEN S-2L AND S-2R). REPAMar 30, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, FrameSDR FDEA201003301034Frame · damagedINTERIOR FRAME WITH DOUBLE HOLE AND CLOSE SPACED HOLES AT BS 395, BETWEEN STR 2L TO STR 2R. FRAME AT STA 395, BETWEEN STR 2L AND 2R REPAIRED IAW EA 757-5312-08-E0612 (EXTRANEOUS FASTENER HOLES FOUND ON STA 395 AND 418 FRAMES, BETWEEN S-2L AND S-2R). REPAIR Mar 30, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, FrameSDR FDEA201003301033Skin · damagedCABIN : ELONGATED SCREW HOLE 02 EA ON FLOORBEAM LWR CHORD AT STA 580, RBL 26. FLOORBEAM LOWER CHORD AT STA 580, RBL 26, SCREW HOLE REPAIRED IAW EA NR F-5310-138510 (ELONGATED NUTPLATE HOLES ON FLOORBEAM LOWER CHORD ON BS 580). REPAIR IS CLASSIFIED AS MAJOR IAMar 30, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/SkinSDR FDEA201003250992Skin · corrodedFUSELAGE EXTERIOR LOWER SKIN WITH SURFACE CORROSION AT LT BS 440 TO BS 660, BELOW STR 26L. CORROSION REPAIR CARRIED OUT ON EXTERIOR FUSELAGE SKIN FROM BS 440 TO BS 660, BELOW STR 26L, IAW STA ENGRG EA F-757-5331-08-E0571 (CORROSION ON EXISTING SKIN PANEL P/NMar 25, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/SkinSDR FDEA201003250991Floorbeam · damagedCABIN - ELONGATED SCREW HOLE 02 EA FLOORBEAM LWR CHORD AT STA 640 RBL 26. REPAIR CARRIED OUT ON FLOORBEAM LWR CHORD AT STA 640, RBL 26 IAW STA ENG EA F-757-5335-08-E0619 REV C (ELONGATED NUTPLATE HOLES FOUND ON STA 640 FLOORBEAM LOWER CHORD). REPAIR IS CLASSIMar 25, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201003230965Frame · crackedFWD CARGO COMPARTMENT AT BS 508 BETWEEN STR 23L AND STR 24L FOUND CRACK ON FRAME WEB. FRAME WEB AT BS 508, BETWEEN STR 23L AND STR 24L REPAIRED IAW EA F-5310-138514. (FRAME WEB CRACK REPAIR AT BS 508, BETWEEN S-23L AND S-24L). REPAIR IS CLASSIFIED AS MAJOR Mar 23, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, FrameSDR FDEA201003230964Floorbeam · noneCABIN - EXISTING DOUBLER REPAIR FOUND ON FLOORBEAM UPPER CHORD AT STA 377 LBL 14. TO EVALUATE. REPAIR CARRIED OUT ON FLOORBEAM UPPER CHORD DOUBLER AT STA 277, FROM LBL 6.8 TO RBL 11.5 IAW EA F-5310-138503 (EXISTING FLOOR BEAM UPPER CHORD REPAIR AT BS 377.70)Mar 23, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201003210973Frame · damagedAT BS 520 BETWEEN STR 25L AND STR 26L, 1 EA EXISTING FASENER HOLE FOUND ELONGATED (0.35") AT THE FLANGE OF FRAME. FRAME AT BS 520, FROM STR 25L TO STR 26L REPAIRED IAW STA ENG EA 757-5332-08-E0573 (INCOMING ELONGATED FASTENER HOLE AT STA 520 FRAME, BETWEEN 25Mar 21, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, FrameSDR FDEA201003210957Skin · unknownAFT CARGO NR 2 CARGO DOOR INNER SKIN BETWEEN BS 1383 TO BS 1388 FOUND WITH PREVIOUS REPAIR. REPAIR ON AFT CARGO DOOR INNER SKIN BETWEEN BS 1383 AND BS 1388 CARRIED OUT IAW EA F-5230-135817 (NR 2 CARGO DOOR INNER SKIN CRACK REPAIR). REPAIR IS CLASSIFIED AS Mar 21, 2010 · N936FD · Boeing 7572T7 · Cargo/Baggage DoorsSDR FDEA201003210956Floorbeam · unknownCABIN FLOORBEAM LOWER CHORD AT STA 700, LBL 40 TO RBL 40 FOUND WITH PREVIOUS REPAIR. REPAIR CARRIED OUT ON CABIN FLOORBEAM LOWER CHORD AT STA 700, FROM LBL 40 TO RBL 40 IAW EA F-5310-138505 (EXISTING LOWER FLOORBEAM LOWER CHORD REPAIR AT BS 700). REPAIR IS CMar 21, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Floor BeamSDR FDEA201003210954Skin · unknownFUSELAGE R4 PASSENGER DOOR CUTOUT WITH EXISTING FRAME REPAIR AT DOOR GUSS LOCK CUTOUT LOWER INBD CORNER, AT BS 1640. TO EVALUATE R4 DOOR CUTOUT FRAME AT DOOR GUST LOCK CUTOUT LOWER INBD CORNER REPAIRED IAW EA NR F-5360-137439 (SECT. 46 RT NR 4 PASSENGER DOORWMar 21, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/SkinSDR FDEA201003210953Skin · crackedLT L4 PASSENGER DOOR WITH EXISTING FRAME REPAIR AT FWD EDGE HOLD OPEN LATCH CUTOUT AT BS 1640. TO EVALUATE, L4 PASSENGER DOOR CUTOUT FWD EDGE HOLD-OPEN LATCH CUTOUT REPAIRED IAW EA F-5360-137434, L4 PASSENGER DOORWAY BS 1640 FRAME WEB REPAIR AT DOOR STOP NR 3Mar 21, 2010 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/Skin
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