Boeing 737-290C

Service difficulty reports · 1,409

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 = '737290C'
  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 ASAA0510323Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR LEFT PRIMARY FORWARD CLEVIS FORWARD FACE. FACES MACHINED PER EA 5340-01138. (M)Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/RibSDR ASAA0510322Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M)Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/RibSDR ASAA0510321Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS AFT FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M)Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/RibSDR ASAA0510320Spar · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 65-46572 AND B737-200 SRM 51-30-2. (M)Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/RibSDR ASAA0510319Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS AFT FACE. CLEVIS REPLACED PER EA 5340-01137. (M)Sep 22, 2005 · N740AS · Boeing 737290C · Vertical Stabilizer, Spar/RibSDR ASAA0510324Clevis · corrodedCORROSION ON VERTICAL STABILIZER AFT SPAR LT FAIL SAFE CLEVIS FACES NOT PARALLEL TO EACH OTHER. FACES MACHINED IAW EA. (K)Sep 22, 2005 · N740AS · Boeing 737290C · Elevator, Spar/RibSDR ASAA0510318Floorbeam · corrodedFOUND EXFOLIATION CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 328, FROM BL 0 -RBL 56. CHORD REPLACED IAW SRM 53-10-9.Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor BeamSDR ASAA0510317Stringer Splice · corrodedYXX - FOUND CORROSION ON STRINGER SPLICE AT BS 370-380 STRINGER 27 RT. STRINGER SPLICE REPLACED PER B737-200 SRM 51-30-2. (M)Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous StructureSDR ASAA0510316Floor Support · corrodedYXX - FOUND CORROSION AT 5 CLIP NUT LOCATIONS ON FLOOR SUPPORT STRUCTURE LOCATED AT LBL 40, WL 207, BS 312-344. FLOOR SUPPORT CHORD REPAIRED BY REPLACEMENT PER B737-200 SRM 51-30-2. (M)Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous StructureSDR ASAA0510315Skin · corrodedYXX - FOUND IN FORWARD CARGO BAY CORROSION ON SKIN AT BS 360-380 AT STRINGER 27 RT. SKIN REPAIRED PER B737-200 SRM 53-30-3. (M)Sep 21, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510314Floorbeam · corrodedYXX - FOUND UPPER CHORD OF BS 344 FLOORBEAM CORRODED FROM RBL 5-10, UNDER FASTENER HEADS AND ON SURFACE. REMOVED AND REPLACED UPPER CHORD PER B737-200 SRM 53-10-9. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor BeamSDR ASAA0510313Floorboard · corrodedYXX - IN FORWARD CARGO PIT CORROSION ON LOWER CHORD OF CABIN FLOOR BOARD AT BS 420 LBL 36-44 BETWEEN PREVIOUS REPAIR PARTS. THE LOWER CHORD OF CABIN FLOORBEAM AT BS 420 FROM LBL 36-44 WAS REPAIRED IAW EA 5310-02491. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Floor PanelSDR ASAA0510312Stringer Splice · damagedYXX - FOUND STRINGER SPLICE AT BS 365-350 AT STRINGER 26 RT HAS ELONGATED HOLES. REPLACED STRINGER SPLICE IAW B737-200 SRM 51-30-5 FIGURE 3. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous StructureSDR ASAA0510311Stringer Splice · damagedYXX - FOUND STRINGER SPLICE AT BS 365 TO 350 AT STRINGER 27 LEFT HAS ELONGATED HOLES. REPLACED STRINGER SPLICE IAW B737-200 SRM 51-30-5 FIGURE 3. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Miscellaneous StructureSDR ASAA0510310Stringer · corrodedYXX - FOUND CORROSION ON STRINGER AT BS 363-375 STRINGER 27 RIGHT. STRINGER 27 RT REPLACED FROM 363 TO 407 IAW B737-200 SRM 53-10-3. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510309Floorbeam · corrodedYXX - FOUND IN FORWARD CARGO PIT LOWER CHORD OF FLOORBEAM CORRODED AT BS 420 LBL 24. LOWER CHORD OF CABIN FLOORBEAM AT BS 420 LBL 24 WAS REPAIRED IAW ERO 4457 AND EA 53110-02491. REF ASA LOG 3017604 FOR WORK DETAILS. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor BeamSDR ASAA0510308Failsafe · cutYXX - FOUND FAIL/SAFE AT BS 360 TO BE CUT FOR ACCESS AT STRINGER 26 RT. REPAIRED IAW B737-200 SRM 51-40-3 FIGURE 1. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, FrameSDR ASAA0510307Attach Angle · corrodedYXX - FOUND CORROSION ON SKIN TO FRAME ATTACH ANGLE BETWEEN STRINGER 28-27 LEFT AT BS 360. SKIN TO FRAME ATTACH ANGLE AT BS 360 BETWEEN STRINGER 27 LEFT AND 28 LEFT REPAIRED PER B737-200 SRM 53-10-4 FIGURE 8. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Internal Mounting StructureSDR ASAA0510306Doubler · corrodedYXX - FOUND CORROSION ON BONDED DOUBLER AT BS 360 BETWEEN STRINGER 26R AND 27R. REPAIRED PER B737-200 SRM 51-40-3. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510305Stringer · corrodedYXX - FOUND CORROSION ON STRINGER 26R AT BS 500A. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510304Stringer · cutYXX - FOUND STRINGER 26L AT BS 334 TO BS 358 CUT. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510303Stringer · damagedYXX - FOUND STRINGER 27L AT BS 395 CUT FOR ACCESS. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510302Doubler · dentedYXX - FOUND DOUBLER DAMAGED AT BS 360 BETWEEN STRINGER 27R TO 28L PLUS 14 INCHES. REPLACED DOUBLER PER B737-200 SRM 57-40-3 FIGURE 1. (M)Sep 20, 2005 · N740AS · Boeing 737290C · Fuselage Main, StructureSDR ASAA0510299Stringer · dentedYXX - IN FORWARD PIT STRINGER 25 LEFT DENTED AT BS 51. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 53-10-03. (M)Sep 15, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510298Stringer · damagedYXX - FOUND TOOLING DAMAGE AT BS 440, STRINGER 7 RT. REPAIRED IAW B737-200 SRM 53-10-3 FIG 4. (M)Sep 15, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510297Stringer · corrodedYXX - FOUND CORROSION ON STRINGER 27 RT AT BS 360. REPAIRED BY REPLACEMENT. (M)Sep 13, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510296Floorbeam · corrodedYXX - FOUND BEYOND LIMITS CORROSION ON BS 807 FLOORBEAM UPPER CAP AT LBL 24-LBL 45. REPAIRED IAW ERO 4554 AND EA 5310-02425 BY REINFORCEMENT OF CAP WITH STRAP. (M)Sep 13, 2005 · N740AS · Boeing 737290C · Fuselage Main, Floor BeamSDR ASAA0510295Skin · corrodedYXX - FOUND FUSELAGE SKIN BULGING AT BS 535 LEFT KEELBEAM. REPAIRED BY REPLACEMENT OF LEFT KEEL BEAM SECTION. (M)Sep 12, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510294Shear Tie · corrodedYXX - FOUND SKIN TO FRAME ANGLE CORRODED AT BS 360 BETWEEN STRINGER 25 RT AND 26 RT. REMOVED AND REPLACED FRAME TO SKIN ATTACH ANGLE PER B737-200 SRM 53-10-04 FIGURE 8. (M)Sep 12, 2005 · N740AS · Boeing 737290C · Fuselage Internal Mounting StructureSDR ASAA0510293Frame · corrodedYXX - FOUND CORROSION ON FRAME TO SKIN ATTACH ANGLE AT BS 360 BETWEEN STRINGER 26-27 RT. REMOVED AND REPLACED FRAME TO SKIN ATTACH ANGLE PER SRM 53-10-4. (M)Sep 12, 2005 · N740AS · Boeing 737290C · Fuselage Main, FrameSDR ASAA0510292Bear Strap · scratchedYXX - FOUND SCRATCHES ON BEAR STRAP AT BS 500 FROM STRINGER 3 LEFT TO 17 LEFT. PLT SUBMITTED. BEAR STRAP AT BS 500 FROM STRINGER 3 LEFT TO 17 LEFT WAS REPAIRED IAW ERO 4283 AND EA 5330-01982. (M)Sep 7, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510291Skin · damagedYXX - FOUND FUSELAGE SKIN DAMAGED AT BS 996 1 INCH BELOW STRINGER 21 LEFT. DAMAGED FUSELAGE SKIN REPAIRED AT BS 996 1 INCH BELOW STRINGER 21 LEFT IAW B737-200 SRM 53-30-3 FIG 48. (M)Sep 7, 2005 · N740AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510290Stringer · dentedYXX - IN FORWARD CARGO PIT STRINGER 25 LEFT DENTED AT BS 408. REPLACED STRINGER PER B737-200 SRM 53-10-3. (M)Sep 7, 2005 · N740AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510173Keelbeam · corrodedYXX - FOUND CORROSION ON RIGHT KEEL BEAM AT BS 636. RIGHT KEEL BEAM REPLACED IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, KeelSDR ASAA0510172Keelbeam · corrodedYXX - FOUND CORROSION ON RIGHT KEEL BEAM AT BS 636. LEFT KEEL BEAM REPLACED IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, KeelSDR ASAA0510171Skin · chafedYXX - FUSELAGE SKIN LEFT BS 262 3.5 INCHES ABOVE NLG DOOR CUTOUT CHAFED. SKIN CHAFED REPAIRED IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510170Rib · wornYXX - FOUND LEFT WING RIB BETWEEN AILERON AND FORE FLAP T/E ANGLE SUPPORT CHANNEL HAS WEAR DAMAGE. REMOVED AND REPLACED SUPPORT ANGLE IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Wing, Rib/BulkheadSDR ASAA0510169Stringer Clip · corrodedYXX - FOUND AFT CARGO PIT TIE CLIP HAS CORROSION AT BS 747 AND STRINGER 26R. REMOVED AND REPLACED TIE CLIP AT AFT CARGO BS 747 AND 26R IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, Attach FittingsSDR ASAA0510168Skin · corrodedYXX - FOUND FUSELAGE SKIN BULGING AT BS 535 STRINGER 28 LEFT KEEL BEAM. REMOVED AND REPLACED KEEL BEAM AND REPAIRED SKIN IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510167Stringer Clip · crackedYXX - FOUND AFT CARGO TIE CLIP CRACKED AT BS 787 STRINGER 24R. REMOVED AND REPLACED TIE CLIP IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Miscellaneous StructureSDR ASAA0510166Keelbeam · damagedYXX - FOUND BS 535 BETWEEN LEFT AND RIGHT KEEL BEAMS SUPPORT ANGLES HAS LOW EDGE MARGIN AT FASTENER HOLE. REMOVED AND REPLACED ANGLE IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, KeelSDR ASAA0510165Angle · damagedYXX - FOUND U-CHANNEL AT AFT CARGO PIT DOOR SILL HAS ELONGATED HOLES FROM PREVIOUS REPAIR. REMOVED AND REPLACED U-CHANNEL IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Miscellaneous StructureSDR ASAA0510164Stringer · crackedYXX - FOUND CRACKED STRINGER AT BS 836 STRINGER 26R. REMOVED AND REPLACED STRINGER 26R IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASAA0510163Wedge · dentedYXX - FOUND RIGHT NR 6 SLAT T/E WEDGE UPPER SURFACE HAS A DENT AT SLAT STATION 346.53 AND 4.5 INCH FROM T/E. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 7 FIG 16. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Leading Edge DevicesSDR ASAA0510162Wedge · dentedYXX - FOUND RIGHT NR 6 SLAT T/E WEDGE UPPER SURFACE HAS A DENT AT SLAT STATION 359.03 AND 1.5 INCHES FROM T/E. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 11 FIG 20. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Leading Edge DevicesSDR ASAA0510161Skin · delaminatedYXX - FOUND RIGHT NR 6 SLAT FS 540, UPPER EDGE HAS DAMAGE. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 14 FIG 23. (M)Jun 14, 2005 · N742AS · Boeing 737290C · Leading Edge DevicesSDR ASAA0510185Stringer · corrodedOB SIDE OF STR 26L AT B-STA 986 CORRODED. REMOVED AND REPLACED STRINGER 26L IAW SRM. (K)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, Longeron/StringerSDR ASA0510184Door Frame · crackedDOOR FRAME ON FUSELAGE IS CRACKED (AFT END FWD FRAME. REPLACED IAW SRM. (K)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, StructureSDR ASAA0510183Skin · corrodedFUSELAGE SKIN BULGE AT B-STRA 535, STR 28, LT. REPAIRED IAW SRM. (K)Jun 14, 2005 · N742AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR ASAA0510182Web · dentedDENT ON WEB ON LT WING RSS 497 APPROX 10 INCHES AFT OF REAR SPAR. REPAIRED IAW SRM. (K)Jun 14, 2005 · N742AS · Boeing 737290C · Wing Miscellaneous Structure
Back to Boeing 737-290C