Boeing 737-490

Service difficulty reports · 3,288

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 = '737490'
  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 ASAA2015073112653Warning Message · false activationDATA LINK FULL MESSAGE, ACFT GROUNDED. RESOLVED IAW QRH.Jul 31, 2015 · N569AS · Boeing 737490 · Flight Management Computing Hardware SystemSDR ASAA2015072912676Stiffener · crackedLEFT HORIZONTAL STABILIZER AT STABILIZER 129.5 RIB, STIFFENER CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND DWG 65-47508, REV C.Jul 29, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer StructureSDR ASAA2015072912675Stiffener · crackedLEFT HORIZONTAL STABILIZER AT STAB STA 129.5 RIB, STIFFENER, PN 65-47508-50 IS CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND BAC DWG 65-47508, REV C.Jul 29, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer StructureSDR ASAA2015072812940Frame · damagedFUSELAGE FRAME BS 727D HAS AN ENLONGATED HOLE AT LT LOWER Z ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED IAW EA 400-53EA-15683, REV NEW.Jul 28, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015072812939Frame · damagedFUSELAGE FRAME 727F HAS AN ENLONGATED HOLE AT LT LOWER Z-ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15684, REV NEW, STA 727F.Jul 28, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015072812620Warning Light · false activationSTARTED APU, HAD BLUE LIGHT "APU GEN OFF BUSS" LIGHT UP BUT NO VOLTS OR FREQUENCIES. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. STARTED APU, BLUE GENERATOR OFF BUSS LIGHT ON WITH GOOD VOLTS AND FREQUENCIES. GROUND VERIFICATION TEST PASSED IAW MM 24-21-00. Jul 28, 2015 · N569AS · Boeing 737490 · AC Generation SystemSDR ASAA2015072312757Web · corrodedAFT CARGO DOOR SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED CORRODED ORIG .045", REMAIN .040" LOSS OF .005", FOUND OUT OF LIMITS IAW SRM 53-60-16, NEW WEB IAW DWG 65-479.57 AND DWG A530001818L. DRILLED AND INSTALLED 2 EA DOUBLERS IAW DWG A5330001818L.Jul 23, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072212933Floor Support · corrodedAFT CARGO BAY LT FLOOR SUPPORT ANGLE IS CORRODED APPROXIMATELY BS 727+4 TO BS 760. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-53-1A-1, ORIGINAL MATERIAL THICKNESS WAS 0.040 IN REMAINING THICKNESS 0.000 IN ACCOMPLISHED SPJul 22, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072212920Strip · corrodedAFT CARGO COMPARTMENT, RT CAP STRIP NR 4, AFT OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS -.063. REMOVED -.012 REMAINING THICKNESS .051 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, MAT ID 2024-T3, PJul 22, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072212756Strip · corrodedAFT CARGO COMPARTMENT, RT CAPSTRIP NR 3, FWD OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL USING TOOL T82254 CAL DATE 11/25/2015, ORIGINAL THICKNESS .063", REMOVED .024" REMAINING THICKNESS .039" FOUND TO BE OUT OF ALLOWJul 22, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112937Frame · crackedCRACK INDICATIONS FOUND BS 520 ABOVE S-21L IN .500" HOLE, MARKED AT 7 & 9 O'CLOCK POSITION IN FWD PIT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15603.Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015072112936Frame · crackedRIGHT BS 500B, .500" WIRE PENETRATION HOLE, ABOVE S-21R HAS CRACK INDICATION DUE TO NOISE. IN FWD PIT, MARKED. ACFT GROUNDED. CLEANED HOLE RT BS 500B, 500" WIRE PREPERATION, HOLE ABOVE S-21R IAW NDT MANUAL PART 6, 51-00-00 PROCEDURE 1, PARA 4, CRACK INDICATJul 21, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015072112934Strip · corrodedPARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED. LT NR 2. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .020 REMAINING THICKNESS .049 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 MATERIAL ID 2024-T3 PJul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112933Strip · corrodedPARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED, RT NR 3. ACFT GROUNDED. REMOVED CORROSION FROM PANEL, ORIGINAL THICKNESS .063. REMAINING THICKNESS .039 FOUND TO BE OUT OF LIMITS WITH MINIMUM THICKNESS REMAINING OF .057 IAW SRM 53-60-53, 10 PERCENTJul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112694Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORROSION LT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .022, REMAINING THICKNESS .041 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112691Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .031, REMAINING THICKNESS .032 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 53-6Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112690Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS 0.63, REMOVED .012, REMAINING THICKNESS .051 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112689Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED RT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKESS .063, REMOVED .013, REMAINING THICKNESS .050 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112688Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED LT NR 4. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063 REMOVED .018. REMAINING THICKNESS .045 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112674Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063. REMOVED .037, REMAINING THICKNESS .026. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRMJul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112673Support · corrodedAFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .011. REMAINING THICKNESS .052 FOUND TO BE PAST 10 PERCENT, ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112672Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .031. REMAINING THICKNESS .032, FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072112671Support · corrodedAFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .024. REMAINING THICKNESS .039. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-0Jul 21, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015072012938Door Frame · gougedAFT CARGO DOOR, FWD DOOR FRAME, 2ND FROM UPPER DOOR STOP PIN FITTING GOUGED. APPROXIMATELY S-21R MARKED IN RED. DOT ATTACHED. ACT GROUNDED. R & R AFT CARGO DOOR FWD FRAME 2ND FROM UPPER STOP FITTING, BEAM B IAW SRM 51-40-02 AND 51-10-02, PARA 8, AND DWG 65-4Jul 20, 2015 · N708AS · Boeing 737490 · Fuselage Main, StructureSDR ASAA2015072012913Stop Fitting · gougedFORWARD CARGO DOOR, FWD DOOR FRAME, UPPER DOOR STOP PIN FITTING GOUGED DEEP. APPROXIMATELY S-20R, MARKED IN RED, DOT ATTACHED. ACFT GROUNDED. R & R CARGO DOOR FWD DOOR FRAME UPPER STOP PIN FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02, DWG 65-46921, REV K REJul 20, 2015 · N708AS · Boeing 737490 · Cargo/Baggage DoorsSDR ASAA2015071812938Frame · crackedBS 500F RT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 6 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500F, S-20R-S-21R IAW EA 400-53EA-15605, REV: NEW.Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071812919Frame · crackedBS 500B, LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500B, S-20L TO S-21L IAW SRM 53-00-07-2R-B.Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071812918Frame · crackedBS 500G, LT FRAME IN FWD CARGO BAY, A .500 INCH HOLE HAS CRACK INDICATION NOTED IN FRAME AT 10 O'CLOCK POSITION. REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIR FUSELAGE FRAME AT BS 500G LT SIDE S-20L TO S-21L IAW SRM 53-00-07-2Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071812871Attach Bracket · gougedFWD CARGO DOORWAY FWD FRAME INTERNAL ATTACH BRACKET GOUGED, STREAMER ATTACHED, STR 24R. ACFT GROUNDED. R & R FWD CARGO DOORWAY, FW FRAME BACKUP FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02 AND BAC DWG 65-20722, REV B, REMOVED DOT N258 .Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, Attach FittingsSDR ASAA2015071812868Frame · crackedBS 500F STRINGERS 20 - 21L FRAME IN FWD CARGO BAY, A .500 HOLE HAS CRACK INDICATION NOTED IN FRAME AT 5 O'CLOCK POSITION. ACFT GROUNDED. REPAIRED THE FRAME IAW SRM 53-00-07-2R-13.Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071812843Frame · crackedBS 500D LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. ACCOMPLISHED REPAIR BS 500D LT FRAME AT .500 HOLE AT STR 20L-STR 21L IAW SRM 53-00-07-2R-13Jul 18, 2015 · N708AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071812833Skin · crackedCRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN, APPROXIMATELY STABILIZER BS 123, APPROXIMATELY 1" IN LENGTH, MARKED IN RED. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN IAW EA 400-55EA-15572, REV NEW AND REO-G19081, REV A.Jul 18, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015071812521Light · inoperativeV NAV LIGHT DOES NOT LIGHT UP. ACFT GROUNDED. DFCS LIBRARY TEST NR 50 SHOWED ALL MCP SWITCH LIGHTS TO BE INOPERATIVE. SUSPECT INTERNAL MCP FAULT. R & R AND TESTED DFCS MODE CONTROL PANEL IAW MM 22-11-34-004-004, MM 22-11-34-404-003. PERFORMED DFCS GROUP NRJul 18, 2015 · N793AS · Boeing 737490 · Autopilot SystemSDR ASAA2015071712915Hinge · crackedFORWARD SERVICE DOOR, LOWER HINGE HAS ONE FASTENER HOLE WITH A CRACK INDICATION. UNABLE TO DETERMINE LAYER. INDICATION POSITIONED AT 11 O'CLOCK IN HOLE, MARKED. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN AND BEAR STRAP COMMON TO FORWARD GALLEY, R1, Jul 17, 2015 · N708AS · Boeing 737490 · Fuselage, Door HingeSDR ASAA2015071712869Fitting · crackedCRACK INDICATION ON LT UPPER, OTBD HORIZONTAL STABILIZER THRUST BEAM CORNER FITTING, APPROX 2" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED REPLACEMENT OF LT SIDE HORIZONTAL STABILIZER THRUST BEAM CORNER FITTINGS IAW EA 400-55EA-15573, REV A.Jul 17, 2015 · N708AS · Boeing 737490 · Horizontal Stabilizer StructureSDR ASAA2015071612937Floorbeam · corrodedAFT CARGO COMPARTMENT, FLOOR PANEL SPLICE TEE AT BS 772 IS CORRODED/EXFOLIATED, PARTS RACK. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-53-1A-1, DETAIL V SECTION B-B. ORIGINAL THICKNESS 0.070, REMOVED 0.014, REMAINING THICKNESS 0.056, FOUND TO BE OUT OF LJul 16, 2015 · N708AS · Boeing 737490 · Fuselage Main, Floor BeamSDR ASAA2015071612934Floorbeam · corrodedAFT CARGO FLOOR PANEL SPLICE TEE AT BS 727F+5 IS CORRODED/EXFOLIATED, PARTS RACK. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-53-1A-1, DETAIL IV SECTION B-13. ORIGINAL THICKNESS 0.070, REMOVED 0.015, REMAINING THICKNESS 0.055, FOUND TO BE OUT OF LIMITS IAJul 16, 2015 · N708AS · Boeing 737490 · Fuselage Main, Floor BeamSDR ASAA2015071612939Cargo Track · corrodedAFT CARGO COMPARTMENT, DOORWAY FLOOR SUPPORT TRACK IS CORRODED/EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-53-1A-1. ORIGINAL MATERIAL THICKNESS WAS 0.090", REMOVED 0.052", REMAINING THICKNESS WAS 0.038". ACCOMJul 16, 2015 · N708AS · Boeing 737490 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2015071612935Channel · corrodedAFT CARGO COMPARTMENT, DOOR SURROUND SHIELD IS CORRODED. ACFT GROUNDED. R & R DOOR SURROUND SHIELD IAW SRM 51-40-02 AND DWG 65-47957 CORROSION, REMOVED AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1. ORIGINAL THICKNESS WAS .050 IN REMOVED 0.0006 INJul 16, 2015 · N708AS · Boeing 737490 · Fuselage Miscellaneous StructureSDR ASAA2015071612832Bear Strap · corrodedAFT CARGO DOOR CUTOUT, AFT SIDE, SKIN BEARSTRAP DOUBLER IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MATERIAL, REMOVED .030" FOUND TO BE OUT LIMITS IAW SRM 53-00-01. REMOVED DOOR THRESHOLD WEB, AFT EDGE COVER STRAP, CORNER EDGE COVER STRAP AND LOWER SILL OJul 16, 2015 · N708AS · Boeing 737490 · Fuselage Main, Plate/SkinSDR ASAA2015071012721Frame · crackedFRAME AT BS 747 IS CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 10, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071012720Frame · crackedFRAME AT BS 727D BETWEEN STR 8 - 9R IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 10, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071012714Frame · crackedFRAME BS 787 BETWEEN STRINGERS 8 - 9R FOUND CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 10, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015071012713Frame · crackedCABIN FRAME AT BS 827 BETWEEN STR 8L AND 9L IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW DATED 14AUG15 WORKFRONT NOTIFICATION SENT TO STRUCTURES ENGINEERING TO ISSUE EC/TC TO ACCOMPLISH 1 TIME INSPECTION THIS IS A DT CATEGJul 10, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015070812719Frame · crackedFRAME AT BS 480 CRACKED BETWEEN S 8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 8, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015070812718Frame · crackedFRAME AT BS 440 CRACKED BETWEEN S8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 8, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015070812717Frame · crackedFRAME AT BS 400 CRACKED BETWEEN S8 - 9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 8, 2015 · N794AS · Boeing 737490 · Fuselage Main, FrameSDR ASAA2015070714495Cargo Track · corrodedAFT CARGO TRACK, RBL 13 IS CORRODED AT BS 764-877. ACFT GROUNDED. REPAIRED AFT PIT CARGO TRACK BS 764-877, RBL 13.8 IAW EA 400, 53EA 15553 AND SRM 53-00-53-2R-2.Jul 7, 2015 · N794AS · Boeing 737490 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2015070712740Cargo Track · corrodedCARGO TRACK RBL 13 IS CORRODED AT BS 764-877. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW EA AND SRM.Jul 7, 2015 · N794AS · Boeing 737490 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2015070712716Frame · crackedFRAME AT BS 400 CRACKED BETWEEN S7 - 8L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.Jul 7, 2015 · N794AS · Boeing 737490 · Fuselage Main, Frame
Back to Boeing 737-490