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 FDEA200906202186Frame · corrodedAT BS 1620, 27L TO 27R, FRAME CORRODED. CORROSION ON FRAME AT BS1620, 24L TO 24R FOUND EXCEEDED SRM DAMAGE LIMITS. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jun 20, 2009 · N933FD · Boeing 75721B · Fuselage Main, FrameSDR FDEA200906202185Intercostal · corrodedKEEL BEAM INTERCOSTAL BETWEEN STA 860 AND STA 900 HAS INTERGRANULAR CORROSION AT LBL 7.0". CORROSION FOUND EXCEEDED SRM LIMITS. INTERCOSTAL WEB BETWEEN STA 680 AMD STA 900 AT LBL 7 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINORJun 20, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906202184Fitting · corrodedRT AIR CONDITIONING UPPER BAY HAS CONNECTING ROD FITTING CORRODED AT STA 975, RBL 52.0". CORROSION ON FITTING FOUND EXCEEDED SRM LIMITS. CONNECTING ROD FITTING AT STA 975, RBL 52.0 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IJun 20, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906202183Bracket · crackedSTA 1701, S-26L TO 27L BRACKET FOUND CRACKED. CRACKED BRACKET AT STA 1701, BETWEEN STR 26L AND 27L REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97.Jun 20, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906192169Bracket · corrodedLINEAR ACCELEROMETER BRACKETS (QTY 02) CORRODED. CORROSION FOUND EXCEEDED SRM LIMITS. QTY 02 ACCELEROMETER BRACKETS REMOVED AND REPLACED IAW SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906192168Angle · crackedAT STA 660 STR 26L FRAME INNER CHORD FASTENER HOLD CRACKED (ANGLE). REMOVED AND REPLACED CRACKED ANGLE IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906192167Seat Track · corrodedPILOT SEAT TRACK (INBD FWD) HAS CORROSION UNDER THE BASE AND AROUND MOUNTING BOLT. PILOT INBD FWD SEAT TRACK REMOVED AND REPLACED IAW AMM 25-11-01 REV.4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906192166Angle · corrodedSTA 1715, LBL 17 INCHES, ANGLE CORRODED. CORROSION FOUND OUT OF SRM DAMAGE LIMITS. ANGLE REPLACED IAW SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906192165Angle · corrodedSTA 1715, LBL 39.50 INCH TO LBL 33.10 INCH, ANGLE CORRODED. ANGLE AT STA 1715, LBL 39.50 INCH TO LBL 33.10 INCH, REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906192164Web · crackedLOWER FLANGE ON MAIN CARGO DECK FLOOR WEB CRACKED AT STA 335, RBL 46 INCHES, AROUND IMPROPERLY BUCKED RIVET. CRACKED INTERCOSTAL AT STA 335, RBL 46 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906192163Fitting · corrodedNR 2 CARGO DOOR MOST FWD LOWER SILL FITTING FOUND CORROSION OUT OF LIMITS. NR 2 CARGO DOOR MOST FWD LOWER SILL FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 19, 2009 · N933FD · Boeing 75721B · Fuselage Main, Attach FittingsSDR FDEA200906182162Panel · crackedLT WING INBD T/E FIXED PANEL AT W STA 330, WIGGLE PLATE ASSY FOUND CRACKED. CRACKED PLATE REPLACED IAW SRM 51-40-02 REV 97 IAW DWG 113N1635. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 18, 2009 · N933FD · Boeing 75721B · Wing, Plate/SkinSDR FDEA200906182161Plate · corrodedRT MLG WHEEL WELL RT ACMP ASSY MOUNTING PLATE CORRODED AT SEVERAL PLACES. CORROSION FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED RIGHT ACMP ASSY MOUNTING PLATE IAW AMM 20-11-00 REV.4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182158Structure · corrodedBS 1664 L4 DOOR RAIN GUTTER CORRODED. CORROSION FOUND BEYOND SRM LIMITS. L4 DOOR RAIN GUTTER REPLACED IAW SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182151Keelbeam · corrodedKEELBEAM LWR CHORD FROM STA 1048 TO STA 1052, RBL 8 HAS CORROSION AROUND 5 RIVETS. EVALUATE AND RECTIFY. REPAIR CARRIED OUT IAW F-5350-129601, AND IAW SRM 51-00-06 AND 53-40-12 REV 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Main, KeelSDR FDEA200906182150Bracket · damagedRADOMED HOLDING ROD MOUNT LT SIDE ANGLE FOUND DAMAGED AT STA 199. EVALUATE AND REPAIR. DAMAGED RADOMED HOLDING ROD MOUNT LT SIDE ANGLE AT STA 199 REMOVED AND REPLACED IAW SRM 54-40-02 REV 97. ANGLE BRACKET FABRICATED IAW DWG 141N7835. PART IDENTIFIED AJun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182149Angle · corrodedCORRODED "L" ANGLE FOUND AT STA 1715 TO 1720, RBL 51. EVALUATE AND REPAIR. CORRODED "L" ANGLE AT STA 1715 TO 1720, RBL 51 REMOVED AND REPLACED WITH NEW "L" ANGLE IAW SRM 51-40-02 REV. 97. FABRICATE REPLACEMENT PART FOR ANGLE 146N5300-22 IAW PL 146N5300 REV Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182148Angle · corrodedCORRODED "L" ANGLE FOUND AT STA 1715, LBL 9.2 TO LBL 15. EVALUATE AND REPAIR. CORRODED "L" ANGLE REMOVED AND REPLACED IAW SRM 51-40- 02 REV. 97. FABRICATE REPLACEMENT PART FOR 146N5240-20 IAW PL 146N5240 REV H AND DWG 146N5240 SH 1 REV. C. PART MARKED AS FX Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182147Stiffener · corrodedLT KEEL BEAM STIFFENER BRACKET FOUND CORRODED AT STA 967, LBL 8. EVALUATE AND REPAIR. CORRODED LT KEELBEAM STIFFENER BRACKET AT STA 967, LBL 8 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. STIFFENER BRACKET FABRICATED IAW PL 2171N6144 SHT. 2 OF 5 AND MFG Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182146Skin · gougedCABIN INTERNAL FUSELAGE SKIN SURFACE AND INTERCOSTAL FLANGE SPLICE HAS A 1.5 INCHES GOUGE AT STA 393, BETWEEN STRINGERS S-13L AND S-14L. FUSELAGE SKIN SURFACE GOUGE MARK REMOVED IAW SRM 53- 00-01 AND FOUND WITHIN LIMIT. INTERCOSTAL FLANGE SPLICE AT STA 393Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Main, Plate/SkinSDR FDEA200906182145Bracket · corrodedWHILE WORKING ON SNRM N01290 FOUND LINEAR ACCELGROMETER BRACKETS CORRODED AT STA 1681, RBL 47.50, WL 208.10. EVALUATE AND REPAIR. ACCELGROMETER BRACKETS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPLACEMENT BRACKETS FABRICATED FOR 284N1705-2 AND 284N1705Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906182144Angle · corrodedCORRODED "L" ANGLE AT STA 1715, LBL 33.10 TO LBL 39.50, REMOVED AND REPLACED WITH A NEW "L" ANGLE IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.Jun 18, 2009 · N933FD · Boeing 75721B · Fuselage Structure (General)SDR FDEA200906182143Floorbeam · corrodedAT STA 780, LBL 51.0, WL 207.1, FOUND QTY 02 ELONGATED HOLES AND CORROSION ON FLOORBEAM UPPER FLANGE. ELONGATED HOLES AND CORROSION ON FLOORBEAM UPPER FLANGE AT STA 580, LBL 51.0, WL 207.1 REPAIRED IAW EA F-5310-129611. REPAIR IS CLASSIFIED AS MINOR IAW GJun 18, 2009 · N933FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA200906182142Tee Fitting · corrodedKEELBEAM LOWER TEE FITTING FOR FAIRING SUPPORT HAS CORROSION AT STA 955, BL0. CORROSION FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED KEELBEAM LOWER FITING IAW B757-200 SRM 51-40-02 REV.97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRIJun 18, 2009 · N933FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA200906172130Angle · corrodedAT BS 1640, LBL 49, WL 208.10 CORROSION FOUND AROUND FASTENER HOLES UPPER FLOORBEAM CHORD LOWER SIDE. EVALUATE AND REPAIR. FLOORBEAM SUPPORT CHORD AT STA 1640, LBL 49, WL 208.10 REPAIRED IAW EA F5310-129615, FUSELAGE-MAIN FRAME CORROSION ON FLOORBEAM UPPER CJun 17, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906172129Structure · corrodedNR 2 PYLON PLATES AND RIVETS CORRODED ON LT AND RT SIDE OF THE PYLON FOR PANEL NR 441AL. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.Jun 17, 2009 · N933FD · Boeing 75721B · Nacelle/Pylon, Main FrameSDR FDEA200906152117Crease Beam · misrepairedUNDOCUMENTED EXISTING REPAIR WAS FOUND ON CABIN RT CREASE BEAM FROM BS 780 TO BS 800, WL 208.10. FOUND NOT IAW STRUCTURAL REPAIR MANUAL. EA F-5300-128608, & EA F-5300-126218,Jun 15, 2009 · N933FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA200906142084Angle · corrodedNR 2 CARGO DOOR CUTOUT PRESSURE SEAL RETAINER FOUND CORROSION AT SEVERAL PLACES AS MARK. NUMBER 2 CARGO DOOR CUTOUT PRESSURE SEAL RETAINER AND ANGLE REMOVED AND REPLACED IN ACCORDANCE WITH DWG 146N6609 REV. J AND SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AJun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142082Tee Fitting · crackedAFTER INSTALLATION OF LT MLG WW SUPPORT CHANNEL, ADJACENT TEE FITTING FOUND CRACKED. LT MLG WW TEE FITTING REMOVED AND REPLACED AS PER SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Main, Attach FittingsSDR FDEA200906142081Plate · corrodedCORRODED COCKPIT ENTRY DOOR KICK PLATE AT STA 310, WL 208.10, LBL20 TO RBL 2. LH OUTBOARD ANCHOR NUT NOT INSTALLED. CORRODED KICKPLATE REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REV. 96. KICK PLATE FABRICATED AS PER DWG 141N5810 SHT 15, REV. E ANJun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142087Angle · corrodedCORRODED "L" ANGLE FOUND AT STA 1715, RBL 0 TO RBL 9.2. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. "L" ANGLE FABRICATED IAW DWG 146N5300 REV C AND PART MARKED IAW GMM 7-0-1001. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142086Support Bracket · crackedLT OTBD T/E MAIN FLAP PN 113N3003-13, SN CA-0206 OTBD CLOSURE RIB AREA AT WBL 561.0 AFT BRACKET WITH RIVET HOLE FOUND CRACKED. EVALUATE AND RECTIFY AS REQUIRED. LT OTBD T/E FLAP OTBD CLOSURE RIB AREA, WBL 561.0 AFT CRACK SUPPORT BRACKET REMOVED AND REPLACEDJun 14, 2009 · N933FD · Boeing 75721B · Wing, Control SurfacesSDR FDEA200906142083Keelbeam · corrodedCORRODED KEEL BEAM CHORD AT STA 950, RBL 8 (FAIRING STRUCTURE). EVALUATE AND RECTIFY. CORRODED KEEL BEAM CHORD AT STA 950, RBL 8 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR AS PE GMM 6-2-100 CRITERIA.Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Main, KeelSDR FDEA200906142080Intercostal · corrodedCORRODED INTERCOSTAL AT STA 1610 TO STA 1620, LBL 4. INTERCOSTAL REMOVED AND REPLACED IAW DWG 146N5451-9 AND SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142079Keelbeam · corrodedLT KEELBEAM HAS CORROSION FROM STA 1100 TO STA 1120, LBL 8. KEELBEAMHAS NINE CORRODED NUT PLATES. EVALUATE AND RECTIFY. CORRODED LT KEELBEAM AT STA 1100 TO STA 1120, LBL 8 FOUND EXCEEDED. ALLOWABLE DAMAGE LIMITS. KEEL BEAM CHORD REMOVED AND REPLACED IAW DWG Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Main, KeelSDR FDEA200906142077Fitting · corrodedKEEL BEAM FITTING HAS CORROSION AT STA 1037, BL 0, WL 133. EVALUATE AND RECTIFY. KEEL BEAM FITTING AT STA 1037, BL 0, WL 133 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142076Tee Fitting · corrodedKEEL BEAM TEE CHORD STRUCTURE HAS CORROSION AT STA 910, RBL 8. EVALUATE AND RECTIFY. KEEL BEAM TEE CHORD AT STA 910, RBL 8 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142075Angle · crackedCRACKED WEB FOUND AT STA 1320 TO STA 1340, LBL 24.75, WL 207.10. TO REPLACE WEB ANGLE. REMOVED AND REPLACE WEB (P/N 140N2506-1) AND ANGLE (PN 140N2505-5) AT STA 1320 TO STA 1340, LBL 24.75, WL 207.10 IAW DWG 140N2506, DWG 140N2505, AND SRM 51-40-02 REV. 96. Jun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142074Angle · corrodedCORRODED WEB ANGLE FOUND AT STA 1320 TO STA 1340, RBL 24.75, WL 207.10. TO REPLACE WEB ANGLE. REMOVED AND REPLACED WEB (P/N 140N2506-1) AND ANGLE (P/N 140N2505) AT STA 1320 TO STA 1340, RBL 24.75, WL 207.10 IAW DWG 140N2506, DWG 140N2505, AND SRM 51-40-02 RJun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906142073Strap · corrodedCORRODED AFT PRESSURE DECK STRAP FOUND AT BS 1680, BL0 TO RBL 15. EVALUATE AND REPAIR. CORRODED PRESSURE DECK STRAP AT BS 1680, BL0 TO RBL 15 REMOVED AND REPLACED IAW DWG 146N5184 AND SRM 51-40-02 REV. 96. PART MARK AS FX 146N5184-6 IAW GMM 7-0-1001. REPAIRJun 14, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122063Support Angle · corrodedAT BS 1560 STR 22L TO 27L SIDEWALL SUPPORT CORRODED. SIDEWALL SUPPORT CHANNEL AT BS 1560 FOUND BADLY CORRODED BEYOND SRM REPAIR LIMITS. SUPPORT CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122062Support Angle · corrodedAT BS 1460 STR 22L TO 26L SIDEWALL SUPPORT ANGLE CORRODED. FOUND CORRODED BEYOND SRM REPAIR LIMITS. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122061Support Angle · corrodedAT BS 1300 STR 21L TO 26L SIDEWALL SUPPORT ANGLE CORRODED. REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122060Support Angle · corrodedAT BS 1360 STR 22R TO 26R, SIDEWALL SUPPORT ANGLE CORRODED. REPLACEMENT PART FABRICATED IAW PL 453N1801 SHT 13 REV Y AND DWG NR 453N1801 SHT 2 REV. B. REPAIR IS CLASSIFIED AS MINOR AS IAW GMM G-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122059Support Angle · corrodedAT BS 1300 STR 22L TO 26L, SIDEWALL SUPPORT ANGLE CORRODED. CORROSION ON SIDEWALL SUPPORT CHANNEL AT BS 1300 FOUND EXCEEDED SRM DAMAGE LIMITS. CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122058Support Angle · corrodedAT BS 1300, STR 22R TO 26R SIDEWALL SUPPORT ANGLE CORRODED. REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906122042Seat Track · corrodedBS 900 TO BS 1070, LBL 45, SEAT TRACK CORRODED. TRACK REMOVED AND REPAIRED IAW SRM 53-00-52 REV. 97. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906122041Seat Track · corrodedBS 900 TO BS1070, LBL 24, SEAT TRACK CORRODED. FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 53-00-52 REV.97. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.Jun 12, 2009 · N933FD · Boeing 75721B · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906112040Hinge · corrodedPANEL 198 MR HAS 2 CORRODED BEARINGS FWD AND AFT CNT ON HINGES. CORROSION ON HINGE FITTING FOUND EXCEEDED LIMITS IN DWG 149N7723 REV. C. HINGE FITTING REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Jun 11, 2009 · N933FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200906112039Floorbeam · corrodedAT BS 1440 RBL 16, FLOOR SUPPORT ANGLE CORRODED. FOUND EXCEEDED SRM LIMITS. ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Jun 11, 2009 · N933FD · Boeing 757200 · Fuselage Main, Floor Beam
Back to N933FD