N933FD

Service difficulty reports · 462

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 = 'N933FD' 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 FDEA200908052911Angle · corrodedAT BS 840, STR 22L, SIDEWALL-TO-SUPPORT ANGLES FOUND CORRODED. CORROSION ON SUPPORT ANGLES FOUND EXCEEDED SRM DAMAGE LIMITS. ANGLES REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Aug 5, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200908052909Floorbeam · corrodedAT BS 840, STR 22R TO 22L, FLOOR SUPPORT BEAM CORRODED. FLOOR SUPPORT FOUND BADLY CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFED AS MINOR PER GMM 6-2-100 CRITERIA.Aug 5, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200908052898Support · corrodedAIR COND RAM AIR INLET FRAME SUPPORT STRUCTURE HAS CORROSION FROM STA 680 TO STA 900, RBL 19.0". CORROSION ON SUPPORT STRUCTURE FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT STRUCTURE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIEAug 5, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200908042887Skin · crackedL2 PAX DOOR UPPER HINGE CUT-OUT HAS A CRACK. CRACK ON L2 PAX DOOR UPPER HINGE CUTOUT FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW E.A. F-5210-12617. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.Aug 4, 2009 · N933FD · Boeing 75721B · Passenger/Crew DoorsSDR FDEA200908042886Skin · crackedR2 PAX DOOR UPPER HINGE CUT-OUT HAS A CRACK. CRACKED CUT-OUT AREA REPAIRED IAW FEDEX E.A. F-5210-126216 (TITLE: R2 DOOR CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.Aug 4, 2009 · N933FD · Boeing 75721B · Fuselage Main, Plate/SkinSDR FDEA200908032885Housing · corrodedRIGHT AIR COND RAM AIR INLET ASSY TORQUE TUBE SUPPORT HOUSING P/N. 213T3701-2 FOUND CORRODED. CORROSION ON SUPPORT HOUSING FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SUPPORT HOUSING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MAug 3, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200908032884Gate · corrodedR2 PAX DOOR BOTTOM DOOR GATE HAS INTERGRANULAR CORROSION. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. R2 PAX DOOR BOTTOM GATE REMOVED AND REPLACED IAW B757-200 AMM 52-11-38 REV. 4. REPAIR IS CLASSIFIED AS MINOR PER GIMM 6-2-100 CRITIERIA.Aug 3, 2009 · N933FD · Boeing 75721B · Service DoorsSDR FDEA200908032872Frame · damagedAFT CARGO FRAME FOUND WITH TOOLING DAMAGE AT BS 1380, BETWEEN STR 25R AND STR 26R. REPAIRED IAW EA F-5360-132602. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Aug 3, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200908032871Skin · damagedTOOL DAMAGE FOUND ON AFT CARGO BAY FUSELAGE SKIN FROM BS 1360 TO 1375, BETWEEN STR 25R AND 26R. REPAIRED IAW EA NR F-5360-132602. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Aug 3, 2009 · N933FD · Boeing 75721B · Fuselage Main, Plate/SkinSDR FDEA200908022870Support Angle · corrodedBS 839, BL 0 FRAME SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE AT BS 839 FRAME FOUND EXCEEDED SRM LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Aug 2, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200908022869Frame · corrodedBS 839 STR 25R TO 27R FRAME CORRODED. CORROSION ON FRAME SPLICE DOUBLER AT BS 839 FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED SPLICE DOUBLER IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Aug 2, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200908022866Gate · corrodedL2 PAX DOOR BOTTOM DOOR GATE HAS INTERGRANULAR CORROSION. CORROSION ON L2 DOOR GATE EXCEEDED SRM ALLOWABLE DAMAGE LIMIT. DOOR GATE REMOVED AND REPLACED IAW AMM 52-11-38 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Aug 2, 2009 · N933FD · Boeing 75721B · Passenger/Crew DoorsSDR FDEA200908012865Skin · corrodedELEVATOR CONTROL ACCESS DOOR (313AL) EDGE CORRODED. CORROSION ON ELEVATOR CONTROL DOOR SKIN FOUND EXCEED SRM DAMAGE LIMITS. DOOR SKIN REPLACED IAW SRM 52-40-01 REV 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Aug 1, 2009 · N933FD · Boeing 75721B · Service DoorsSDR FDEA200908012864Frame · damagedAT BS 1580 STR 23L FRAME DAMAGED. DAMAGED FRAME REPAIRED IAW SRM 53-00-07 REV 97 FIG 201 DETAIL III. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Aug 1, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200908012863Frame · corrodedAT BS 1400 STR 24L TO 26L FRAME CORRODED AND DAMAGED. CORROSION ON FRAME FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW SRM 53-00-07 REV 97, FIG 201 DETAIL III. TO RE-INSPECT REPAIR AT 37,500 FC AND REPEAT AT 12,000 FC INTERVAL. REPAIR Aug 1, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200907302847Skin · corrodedRT WING SLAT NR 7 T/E WEDGE TOP SKIN INTERNAL SURFACES FOUND WITH CORROSION AS MARKED. RT WING SLAT NR 7 REPAIRED IAW SRM 51-30-01 REV 97. REFER FORM 8130-3 TRACKING NR FA 2009/0327. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CITERIA.Jul 30, 2009 · N933FD · Boeing 75721B · Leading Edge DevicesSDR FDEA200907302846Wedge · dentedMINOR DENT FOUND ON NR 7 SLAT UPPER SKIN AT OSS 333.3 AS MARKED. RT WING NR 7 SLAT T/E WEDGE REPLACED. REF TO FORM F8130-3 TRACKING NR SNF C187867 002. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jul 30, 2009 · N933FD · Boeing 75721B · Leading Edge DevicesSDR FDEA200907302845Wedge · dentedMINOR DENT FOUND ON SLAT NR 7 UPPER SURFACE SKIN AT OSS 344.5 AS MARKED. RT WING NR 7 SLAT T/E WEDGE REPLACED. REFER TO REPAIR DIVISION FORM 8130-3 TRACKING NR NSF C187867 002. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jul 30, 2009 · N933FD · Boeing 75721B · Leading Edge DevicesSDR FDEA200907302844Skin · corrodedRT WING SLAT NR 8 ANGLE FASTENER HOLES THRU ACCESS PANEL 623GB AT OSS 559.55 AND OSS 549.7 FOUND WITH MINOR CORROSION. SLAT NR 8 INTERIOR CORROSION AREA BETWEEN OSS 559.55 AND OSS 549.97 REPAIRED IAW SRM 51-10-02 REV 97. REFER TO FORM 8130-3 TRACKING NR FA 2Jul 30, 2009 · N933FD · Boeing 75721B · Leading Edge DevicesSDR FDEA200907302843Floorbeam · damagedTO COMPLY WITH EA F-5310-129611 REV A, REPAIR ELONGATED HOLES ON FLOORBEAM AT BS 780, LBL 51.0. REPAIR CARRIED OUT ON FLOORBEAM IAW EA F-5310-129611 REV A. REPAIR ELONGATED HOLES ON FLOORBEAM AT BS 780, LBL 51.0. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-10Jul 30, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907302842Floorbeam · corrodedSTA 1681, RBL 47.5 INCH FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON FLOORBEAM FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226, CORROSION ON FLOORBEAM 1681.80, MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS Jul 30, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907302841Floorbeam · corrodedSTA 1681, LBL 39.50 INCH FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON FLOORBEAM FOUND EXCEEDED SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226, CORROSION ON FLOORBEAM 1681.80 AT MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJJul 30, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907302840Floorbeam · corrodedSTA 1681 LBL 32 IN FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON UPPER CHORD FOUND EXCEEDED SRM ACCEPTABLE LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226, CORROSION ON FLOORBEAM 1681.80 AT MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJOR IAJul 30, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907302839Floorbeam · corrodedSTA 1681, LBL 11.50 FLOORBEAM UPPER CHORD BOTTOM CORRODED. CORROSION ON FLOORBEAM UPPER CHORD FOUND EXCEEDED SRM LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226. CORROSION ON FLOORBEAM 1681.80 AT MULTIPLE LOCATIONS - REPAIR. REPAIR IS CLASSIFIED AS MAJOR, GJul 30, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907302838Floorbeam · corrodedAT BS 1680 LBL 53 BOTTOM OF TOP CHORD OF AFT PRESSURE DECK CORRODED. FLOORBEAM UPPER CHORD CORROSION FOUND EXCEEDED SRM REPAIR LIMITS. REPAIR CARRIED OUT IAW EA F-5310-126226. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jul 30, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907282804Channel · corrodedBS 1620, BL 0, STRINGER SPLICE PLATE CORRODED. CORROSION ON STR SPLICE PLATE FOUND EXCEEDED SRM REPAIRABLE LIMITS. SPLICE CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 28, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907282803Stringer · corrodedAT BS 1620 STR 30 BL 0 CORRODED. CORROSION ON STRINGER FOUND EXCEEDED SRM DAMAGE LIMITS. STR 30 BETWEEN STA 1610 AND STA 1620 REPAIRED IAW SRM 53-00-53 REV. 97, REPAIR 2, FIG 207. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 28, 2009 · N933FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200907282802Attach Bracket · corrodedWING-TO-BODY FAIRING SUPPORT FRAME HAS WIRE BUNDLE CLIPS CORRODED AT STA 900. CORRODED WIRE BUNDLE CLIPS ( 7 EA) AT STA 900 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 28, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907282801Frame · damagedLT FRAME STA 1280 FROM STR 10L TO STR 14L, SEVERAL NICKS AND GOUGE MARKS FOUND AT FWD SIDE OF FRAMES. DAMAGED FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV.97 REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 28, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200907272775Panel · corrodedSTA 1200 TO STA 1310 RT TRANSITION PANEL FOUND CORRODED. CORROSION ON TRANSITION PANEL FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 27, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907272774Support Fitting · corrodedKEEL BEAM ACCESS PANEL 149EL ATTACHED HOLD-OPEN ROD SUPPORT FITTING HAS SURFACE CORROSION. CORROSION ON SUPPORT FITTING FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED SUPPORT FITTING IAW AMM 20-11-00 REV. 04. REPAIR IS CLASSIFIED AS MINOR IAW GMM Jul 27, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907272773Retainer · corrodedLT MLG DOOR SEAL RETAINERS AND HARDWARE ARE CORRODED FROM STA 1180 TO STA 1040, LBL 8 BELOW KEEL BEAM. CORROSION ON RETAINERS FOUND EXCEEDED ALLOWABLE SRM DAMAGE LIMITS. RETAINERS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR Jul 27, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907272772Panel · corrodedAT BS 1310 TO 1410 LT SIDE TRANSITION PANEL CORRODED. CORROSION ON TRANSITION PANEL FOUND EXCEEDED SRM REPAIRABLE LIMITS. PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97.Jul 27, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907272771Stop Fitting · gougedNR 1 CARGO DOOR AFT DOOR FRAME, 4TH DOOR STOP FROM TOP HAS A DEEP GOUGE. EVALUATE AND RECTIFY. NR 1 CARGO DOOR, 4TH DOOR STOP FITTING GOUGE AND CORROSION REMOVED AND FOUND TO BE OUT OF LIMIT IAW SRM 52-30-02 REV. 97. DOOR STOP FITTING REMOVED AND REPLACEJul 27, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907272770Floorbeam · corrodedBS 1661 RBL 55 TOP OF FLOORBEAM FOUND CORRODED. EVALUATE AND REPAIR. REPAIRED FLOORBEAM AT BS 1661 RBL 55 IAW PTF STA ENGRG EA NR 757- 5361-08-E0277 REV. -, CORROSION ON FLOORBEAM UPPER CHORD AT STA 1661 RBL 58.22 AFFECTING INSTALLATION OF STIFFENER AND SHJul 27, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907272769Bracket · damagedRT AIR COND UPPER BAY SUPPORT BRACKET AT BS 918, RBL 10" FOUND BADLY DEFORMED. DEFORMED BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Jul 27, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907252755Fitting · corrodedKEELBEAM ACCESS PANEL 149CL ATTACHED HOLD-OPEN ROD SUPPORT PANEL FITTING FOUND CORRODED. CORROSION ON SUPPORT FITTING AT STA. 1085, LBL 8 FOUND EXCEEDED SRM LIMITS. SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV. 4. REPAIR IS CLASSIFIED AS MINORJul 25, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907252754Support Fitting · corrodedKEELBEAM ACCESS DOOR HOLD-OPEN ROD SUPPORT FITTING AT STA 1087, LBL 8, FOUND CORRODED. CORRODED SUPPORT FITTING AT STA 1087 BLENDED AND FOUND EXCEEDED SRM REPAIRABLE LIMITS. SUPPORT FITTING REMOVED AND REPLACED IAW AMM 20-11-00, REV. 4. REPAIR IS CLASSIFIEDJul 25, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907252749Angle · corrodedTEE CHORD ATTACHING SPLICE ANGLE AT STA 918, LBL 8 IN HAS CORROSION. CORROSION ON SPLICE ANGLE FOUND EXCEEDED ALLOWABLE SRM LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jul 25, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907252742Tee Fitting · corrodedAT STA 1240, STR 28L BELOW TRANSITION PANEL SUPPORT TEE CLIP FOUND CORRODED. CORROSION ON CLIP FOUND EXCEEDED SRM LIMITS. CLIP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jul 25, 2009 · N933FD · Boeing 75721B · Fuselage Main, Attach FittingsSDR FDEA200907252741Frame · corrodedWING-TO-BODY FAIRING FRAME AT STA 800, BL0 TO RBL 11 HAS EXFOLIATION CORROSION. WING-TO-BODY FRAME AT STA 800 FOUND CORRODED BEYOND SRM DAMAGE LIMITS. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIJul 25, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200907252740Retainer · corrodedRT MLG DOOR SEAL RETAINERS AND HARDWARE HAVE CORROSION FROM STA 1180 TO STA 1040, RBL 8.0 INCHES BELOW BEAM. CORROSION ON SEAL RETAINERS FOUND EXCEEDED SRM LIMITS. SEAL RETAINERS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IJul 25, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907252739Strap · corrodedAT BS 1560 RBL 26, CARGO CEILING SUPPORT STRAP CORRODED. CORROSION ON STRAP FOUND EXCEEDED SRM LIMITS. STRAP REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jul 25, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907242738Channel · corrodedSUPPORT CHANNEL FOR TRANSITION PANEL ON AFT SIDE OF FRAME AT STA 1640 ABOVE STRINGER 27 RT, CORRODED. CORROSION ON SUPPORT CHANNEL FOUND EXCEEDED SRM LMITS. SUPPORT CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMMJul 24, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907222696Floorbeam · corrodedSTA 1320, RBL 24.75, WL 207.1, FLOORBEAM TOP FLANGE FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-51, FIG 201. REV 96 AND EA F-5310-129614. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 22, 2009 · N933FD · Boeing 75721B · Fuselage Main, Floor BeamSDR FDEA200907172660Intercostal · corrodedFROM BS 1500 TO BS 1520, RBL 4, INTERCOSTAL CORRODED. CORROSION ON INTERCOSTA REMOVED AND FOUND OUT OF SRM LIMITS. INTERCOSTAL REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jul 17, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907172659Support · corrodedAT BS 1440 BETWEEN STR 29R AND 30R, FRAME SUPPORT PLATE CORRODED. CORROSION FOUND OUT OF SRM LIMITS. SUPPORT PLATE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jul 17, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907172658Angle · corrodedFROM STA 1540 TO STA 1560, STR 27L, INTERCOASTAL SUPPORT ANGLE CORRODED. CORROSION FOUND OUT OF SRM ALLOWABLE DAMAGE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jul 17, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907172657Angle · corrodedFROM STA 1360 TO STA 1380, STR 27L, INTERCOASTAL SUPPORT ANGLE CORRODED. CORROSION FOUND EXCEEDED SRM REPAIRABLE LIMITS. SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jul 17, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200907172656Angle · corrodedAT STA 1540 TO STA 1560 STR 26R INTERCOSTAL SUPPORT ANGLE CORRODED. CORROSION ON SUPPORT ANGLE FOUND EXCEEDED SRM ALLOWABLE LIMITS. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-00 CRITERIA.Jul 17, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous Structure
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