Boeing 757-21B

Service difficulty reports · 1,078

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 aircraft_model_key = '75721B'
  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 FDEA200910283703Stringer · corrodedSTR 8L BETWEEN STA 1862 AND STA 1885 CORRODED. EVALUATE AND RECTIFY. STR 8L BETWEEN STA 1862 AND STA 1885, CORROSION ON STR FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II, FIG 101 REV. 98, ORIGINAL MATERIAL THICKNESS IS 0.080" AND REMAINING MATERIAL IS 0.060Oct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910283702Stringer · corrodedSTR 7L BETWEEN STA 1862 AND STA 1885 CORRODED. EVALUATE AND RECTIFY. STR 7L BETWEEN STA 1862 AND STA 1885, CORROSION ON STR FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II, FIG. 101 REV. 98, ORIGINAL MATERIAL THICKNESS IS 0.080" AND REMAINING MATERIAL IS 0.061Oct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910283701Stringer · crackedSTR 6L BETWEEN STA 1862 AND STA 1885 CORRODED. EVALUATE AND RECTIFY. STR 6L BETWEEN STA 1862 AND STA 1885, CORROSION ON STR FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II, FIG. 101 REV. 98, ORIGINAL MATERIAL THICKNESS IS 0.071" AND REMAINING MATERIAL IS 0.055Oct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, StructureSDR FDEA200910283700Stringer · corrodedSTR 5L BETWEEN STA 1862 AND STA 1885 CORRODED. EVALUATE AND RECTIFY. STR 5L BETWEEN STA 1862 AND STA 1885, FOUND WITH CORROSION CRACK. NEW STR FABRICATED IAW DWG NR 148N3123 SHT 1 REV. A AND PL REV A. STR REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIOct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910283699Stringer · corrodedSTR 4L BETWEEN STA 1862 AND STA 1885 CORRODED. EVALUATE AND RECTIFY. STR 4L BETWEEN STA 1862 AND STA 1885, CORROSION ON STR FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II, FIG. 101 REV. 98, ORIGINAL MATERIAL THICKNESS IS 0.050" AND REMAINING MATERIAL IS 0.Oct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910283698Stringer · corrodedSTR 3L BETWEEN STA 1862 AND STA 1885 CORRODED. EVALUATE AND RECTIFY. STR 3L BETWEEN STA 1862 AND STA 1885, FOUND WITH CORROSION CRACK. NEW STR FABRICATED FROM EXTRUSION BAC 1498-141 IAW DWG NR 148N3123 SHT 1, REV A AND PL REV A. STRINGER REPLACED IAW SRM 5Oct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910283697Stringer · corrodedSTR 2L CORRODED BETWEEN STA 1862 AND STA 1885. EVALUATE AND RECTIFY. STR 2L BETWEEN STA 1862 AND STA 1885 FOUND OUT OF LIMITS IAW SRM 43-00-003, DETAIL II FIGURE 101 REV. 98. ORIGINAL MATERIALS 0.045", REMAINING 0.022". NEW STR FABRICATED IAW DWG118 SHT 1Oct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910283696Stringer · corrodedSTR 1 CORRODED BETWEEN STA 1862 AND STA 1885. CORRODED STR 1 BETWEEN STA 1862 AND STA 1885, FOUND WITH CRACK. NEW STR FABRICATED FROM EXTRUSION BAC1498-143 IAW DWG NR 148N3123 SHT 1, REV A AND PL REV A, STR REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSOct 28, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910263667Fairing · gougedNUMBER 2 PYLON AFT STRUT FAIRING LOWER FOUND 2 GOUGED MARKS. REPAIR CARRIED OUT IAW EA NR F-5480-131057. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.Oct 26, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910263666Plate · gougedNUMBER 1 PYLON AFT STRUT FAIRING LOWER PLATE FOUND 2 GOUGED MARKS. REPAIR CARRIED OUT IN ACCORDANCE WITH EA NR F-5480-131057 EA. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.Oct 26, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon, Main FrameSDR FDEA200910263665Support · corrodedRIGHT WING AILERON, OUTBOARD HINGE NR 5 SUPPORT CORRODED AT WS 817. REPAIRED AS PER EA NR F-5710-133416. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 CRITERIA.Oct 26, 2009 · N934FD · Boeing 75721B · AileronsSDR FDEA200910263664Tee Fitting · corrodedFAIRING SUPPORT STRUCTURE: LOWER KEELBEAM VERTICAL WEB TEE FITTING HAS CORROSION AT STA 955, LBL 5.5 TO RBL 5.5. CORRODED TEE FITTING AT STA 955, LBL 5.5 TO RBL 5.5 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOOct 26, 2009 · N934FD · Boeing 75721B · Fuselage Main, Attach FittingsSDR FDEA200910263663Tee Fitting · corrodedKEELBEAM FAIRING SUPPORT STRUCTURE LOWER TEE HAS CORROSION AT STA 901, LBL 7.0". CORRODED TEE FITTING ON KEELBEAM FAIRING SUPPORT AT STA 901 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REAPIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Oct 26, 2009 · N934FD · Boeing 75721B · Fuselage Main, Attach FittingsSDR FDEA200910243649Support · corrodedFAIRING SUPPORT STRUCTURE LOWER T-CHORD HAS CORROSION FROM BS 952.5 TO BS 965 LBL 7.0". BLENDED OUT OF LIMITS, REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.Oct 24, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213643Door Frame · looseR2 DOOR UPPER HINGE OPENING HAS LOOSE FASTENERS AT OLD REPAIR. R2 UPPER HINGE OPENING REPAIRED IAW EA F-5210-133427 (R2 DOOR CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Main, StructureSDR FDEA200910213642Door Frame · crackedL2 DOOR UPPER HINGE OPENING HAS CRACK. CRACKED L2 DOOR UPPER HINGE OPENING REPAIRED IAW EA F-5210-133417 (L2 DOOR CRACK REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Main, StructureSDR FDEA200910213638Web · corrodedAFT CARGO COMPARTMENT WEB BETWEEN STA 1360 AND 1380 CORRODED. STRINGER 27R. CORRODED WEB BETWEEN STA 1360 AND STA 1380 REMOVED AND REPLACED IAW SRM 51-40- 02 REV. 98. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213635Stiffener · corrodedKEELBEAM AFT SECTION STRUCTURE ACCESS PANEL NR 149GL, STIFFENER CORRODED. EVALUATE AND RECTIFY. CORRODED STIFFENER ON ACCESS PANEL NR 149GL. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213634Seat Track · corrodedMAIN CABIN BS 1320 TO BS 1540, LBL 24 SEAT TRACK CORRODED. REMOVED AND REPLACED WITH A NEW REPAIR SEAT TRACK IAW SRM 53-00-52 REV. 98 FIG. 201. THIS RPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910213633Rib · corrodedLT WING AILERON OTBD T/E UPPER CLOSURE RIB HAS CORROSION. LT WING AILERON OTBD T/E UPPER CLOSURE RIB REPAIRED IAW EA F-5740-132615, WINGS-ATTACHED FITTINGS-LT AILERON RIB ASSY HINGE NR 1 REPAIR. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 75721B · Wing, Rib/BulkheadSDR FDEA200910213632Support · corrodedRT FWD WING-TO-BODY FAIRING SUPPORT STRUCTURE FRAME HAS A CORROSION AT BS 840, RBL 0 TO RBL 39. RT FWD WING-TO-BODY FAIRING SUPPORT STRUCTURE FRAME AT BS 840. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR AS IAW GMM 6-2-10Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213631Support · corrodedRT FWD WING-TO-BODY FAIRING, LIGHTING HOLE PLATE AT SUPPORT FRAME HAS A CORROSION AT BS 840, RBL 0 TO RBL 4. EVALUATE AND RECTIFY. RT FWD WING-TO-BODY FAIRING SUPPORT FRAME AT BS 840 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213630Support · corrodedRT WING-TO-BODY FAIRING SUPPORT FRAME HAS A CORROSION AT BS 840, BL 0 TO RBL 50. EVALUATE AND RECTIFY. RT WING TO BODY FAIRING SUPPORT FRAME AT BS 840 REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213629Strap · corrodedAFT CARGO COMPARTMENT FLOOR PLATE SPLICE STRAP AT BS 1510 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910213628Strap · corrodedAFT CARGO COMPARTMENT FLOOR PLATE SPLICE STRAP AT BS 1470 FOUND CORRODED. FOUND OUT OF LIMIT IAW SRM 53-00-53 REV 98 AFTER CORROSION REMOVAL. CORRODED STRAP REPLACES IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 21, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910203621Tee Fitting · corrodedFAIRING SUPPORT STRUCTURE LWR T-CHORD AT BS 996, LBL 6.5" HAS CORROSION. CORRODED LWR T-CHORD FROM STA 967 TO STA 1003. REMOVED AND REPLACED IAW SRM 51-40-02, REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 20, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910203613Tee Fitting · corrodedFAIRING SUPPORT STRUCTURE : LWR TEE FITTING AT STA 995, LBL 4.0" TO RBL 4.0" HAS CORROSION. CORRODED TEE FITTING ON FAIRING SUPPORT STRUCTURE AT STA 995, LBL 4.0" TO RBL 4.0". REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAWOct 20, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910203612Support · corrodedFAIRING SUPPORT STRUCTURE : KEELBEAM LWR VERTICAL WEB ANGLE SUPPORT HAS CORROSION AT BS 908, LBL 5.50", RBL 5.50". CORRODED ANGLE SUPPORT AT BS 908 KEEL BEAM LWR WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-1Oct 20, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910163591Crease Beam · damagedMAIN CABIN BS 1634, RBL 60 CREASE BEAM FASTENER HOLE ELONGATED. REPAIR CARRIED OUT ON BEAM IAW STA, EA 757-5361-08-E0439 REV.- (ELONGATED HOLE FOUND ON 146N8722-43 CHORD, STA 1620 TO 1640 RT). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Oct 16, 2009 · N934FD · Boeing 75721B · Fuselage Main, StructureSDR FDEA200910153589Plate · corrodedFWD CARGO BS 700 TO 720 LAV SERVICE CONTAINER UPPER PLATE CORRODED. CORRODED DOUBLER PLATE ON LAV SERVICE CONTAINER AT BS 700 TO 720. REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 15, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143565Angle · crackedMAIN ACFT BATTERY TRAY AFT VERTICAL SUPPORT ANGLE CRACKED AT STA 259, RBL 14. REMOVED AND REPLACED CRACKED BATTERY TRAY AFT VERTICAL SUPPORT ANGLE IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143568Mount Bracket · crackedFWD NOSE COMPARTMENT, RT BATTERY PACK INBD BOTH MOUNTING BRACKETS CRACKED BS 260 AND BS 247. CRACKED MOUNTING BRACKETS AT FWD NOSE COMPARMTMENT RT BATTERY RACK. REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRIOct 14, 2009 · N934FD · Boeing 75721B · Fuselage Main, Attach FittingsSDR FDEA200910143567Sill · corrodedL3 EMERGENCY LWR SILL UNDERSIDE HAS CORROSION AT STA 1323, RBL 59 APPROX. AT STA 1328, RBL 59 APPROX. CORRODED L3 EMERGENCY DOOR LWR SILL WEB REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143566Gate · corrodedL1 DOOR LWR GATE HAS CORROSION. REMOVED AND REPLACED IAW AMM 52-11-38, REV. 5. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Passenger/Crew DoorsSDR FDEA200910143564Stringer · corrodedAFT CARGO BS 1360 TO 1380 STR 28R CORRODED. CORROSION REPAIR ON STRINGER 28R CARRIED OUT IAW EA NR F-5310-131055.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Main, Longeron/StringerSDR FDEA200910143563Doubler · corrodedSTA 1860 UPPER BULKHEAD LWR SURFACE DRAIN HOLE RBL 13" DOUBLER CORRODED. STA 1860 UPPER BULKHEAD LWR SURFACE DRAIN HOLE CORRODED DOUBLER. REMOVED AND REPLACED IAW SRM 51-40-02. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Main, BulkheadSDR FDEA200910143562Support · corrodedLT WING (TOP) OVERWING FAIRING SUPPORT ASSY HAS CORROSION AT 2 NUTPLATE HOLES AT BS 939. CORRODED LT OVERWING FAIRING SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02, REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143561Support · corrodedKEELBEAM FAIRING SUPPORT STRUCTURE UPPER CHORD HAS EXFOLIATION CORROSION FROM BS 900 TO BS 938, RBL 1.0". FAIRING SUPPORT STRUCTURE REPAIRED IAW EA NR F-5320-133413 (SURFACE CORROSION BLEND OUT REPAIR ON KEEL BEAM FAIRING SUPPORT). REPAIR IS CLASSIFIED AS MINOct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143560Support · corrodedKEELBEAM FAIRING SUPPORT STRUCTURE HORIZONTAL WEB HAS CORROSION AT BS 1079, RBL 5.0". KEELBEAM FAIRING SUPPORT REPAIRED IAW EA NR F-5320-133413 (SURFACE CORROSION BLEND OUT REPAIR ON KEEL BEAM FAIRING SUPPORT). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143559Support · corrodedKEELBEAM FAIRING SUPPORT STRUCTURE HORIZ WEB HAS CORROSION BETWEEN BS 1050, RBL 6.0" AND LBL 6.0". SUPPORT STRUCTURE REPAIRED IAW EA NR F-5320-133413. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143558Support · corrodedFAIRING SUPPORT STRUCTURE, LWR CHORD HAS CORROSION BETWEEN BS 1050 TO BS 1060, RBL 6.00". REPAIR ON SUPPORT STRUCTURE CARRIED OUT IAW EA F-5320-133413. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage Miscellaneous StructureSDR FDEA200910143555Seat Track · corrodedAT LBL 45.50 FROM STA 440 TO STA 680 SEAT TRACK FOUND CORROSION. CORRODED SEAT TRACK FROM STA 440 TO STA 680 REMOVED AND REPLACED IAW SRM 53-00-52 REV 98. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910123540Channel · crackedNR 2 PYLON LBL 12.5", PP STA 170, PP WL 157 HAS A HORIZONTAL FORMED U ANGLE CRACKED. CRACKED U-CHANNEL ON NR 2 PYLON AT PP STA 170, LBL 12.5", PP WL 157, REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910123539Stiffener · crackedNR 2 PYLON OTBD SKIN AT PP STA 185.35, WL 151.33 STIFFENER PN 311N5220-56 FOUND CRACKED AT TOP CORNER. (APPROX. 0.75" LENGTH) CRACKED STIFFENER ON NR 2 PYLON AT PP STA 185.35, WL 151.33, REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MIOct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910123538Stiffener · crackedNR 2 PYLON RBL 13", PP STA 185, PP WL 160 HAS A VERTICAL STIFFENER L ANGLE CRACKED. CRACKED STIFFENER ON NR 2 PYLON AT PP STA 185, RBL 13", PP WL 160, REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910123537Support · crackedNR 1 PYLON PP STA 169 RBL 13", PP WL 160, HAS A FORMED EXTRUSION CRACKED. NUT PLATES ATTACHED. CRACKED FORMED SUPPORT ON NR 1 PYLON AT PP STA 169, RBL 13", WL 160, REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 Oct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910123536Channel · crackedNR 2 PYLON U CHANNEL PP STATION 170 TO PP STATION 185, LBL 13" PP WL 164, HAS A CRACK AT LBL 13" AT LOWER SCREW HOLE. CRACKED CHANNEL ON NR 2 PYLON FROM PPSTA 170 TO PP STA 185, LBL 13" TO RBL 13" , PP WL 164. REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. ROct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910123535Angle · crackedNR 1 PYLON RBL 12.5, PP STATION 171, PP WL 161 HAS L-ANGLE CRACKED. CRACKED ANGLE ON NR 1 PYLON AT PPSTA 171, RBL 12.5 REMOVED AND REPLACED IAW SRM 51- 40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910123534Angle · crackedNR 2 PYLON, LBL 12.5", PP STA 169, PP WL 158 HAS A VERTICAL ANGLE CRACKED. CRACKED ANGLE ON NR 2 PYLON AT PP STA 169, LBL 12.5". REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 12, 2009 · N934FD · Boeing 75721B · Nacelle/Pylon Miscellaneous StructureSDR FDEA200910093521Seat Track · corrodedMAIN CABLE BS 365 RBL 45 SEAT TRACK CORRODED. CORRODED SEAT TRACK AT BS 365, RBL 45. REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 9, 2009 · N934FD · Boeing 75721B · Fuselage, Seat/Cargo Attach Fittings
Back to Boeing 757-21B