Boeing 737-990ER
Service difficulty reports · 10,323
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 = '737990ER' 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.
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 = '737990ER' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2025083061091Floor Panel · delaminatedIN FWD GALLEY, FLOOR PANEL HAS DELAMINATION & AN AREA OF CORROSION IN FASTENER HOLE. GROUNDED - YES. APPLIED PERMANENT REPAIRS TO DAMAGED AREAS OF FLOOR BOARD 141A5810-768 IAW SRM 53-00-50-2R-0, & SRM 53-00-50-2R-7.SDR ASAA2025083060956Floor Support · corrodedIN FWD GALLEY, 5 INCHES FWD OF STA 312, LBL 12, EVIDENCE OF CORROSION ON FLOOR STRUCTURE (MARKED IN RED) GROUNDED - YES. BLENDED AREA, ORIGINAL THICKNESS .180", MATERIAL REMOVED .069", REMAINING THICKNESS .111", FOUND TO BE OUT OF LIMITS IAW B737-900ER 53-10-SDR ASAA2025083060793Floor Panel · delaminatedMULTIPLE AREAS OF DELAMINATION AND MULTIPLE BROKEN FASTENERS ON FLOORBOARD P/N: 147A5810-445. GROUNDED - YES. REPAIRED DELAMINATION AND REPLACED INSERTS ON FLOORBOARD P/N: 147A5810-445 IAW B737-900 SRM 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2025083060790Floor Panel · delaminatedMULTIPLE CORRODED FASTNERS AND AREAS OF DELAMINATION ON FLOORDBOARD 241ABF P/N: 147A5810-439. GROUNDED - YES. REPAIRED DELAMINATION AND REPLACED FASTENERS ON FLOORBOARD 241AF P/N: 147A5810-439 IAW B737-900 SRM 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2025083060785Floorboard · delaminatedMULTIPLE CORRODED FASTNERS AND AREAS OF DELAMINATION ON FLOORBOARD 242TF. GROUNDED - YES. REPAIRED DELAMINATION AND REPLACED INSERTS ON FLOORBOARD 242TF IAW B737-900 SRM 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2025083060782Floorboard · delaminatedMULTIPLE CORRODED FASTENERS AND AREAS OF DELAMINATION ON FLOORBOARD 241ADF P/N: 147A5810-443. GROUNDED - YES. REPAIRED DELAMINATION AND REPLACED INSERTS ON FLOORBOARD 241ADF P/N:147A5810-443 IAW B737-900 SRM 53-00-50-2R-1, 53-00-50-2R-1.SDR ASAA2025082961089Landing · corrodedFWD CARGO AFT RT BULKHEAD PANEL LANDING IS CORRODED BEYOND REPAIR. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO AFT RT BULKHEAD PANEL LANDING IAW B737-900ER SRM 51-40-02 AND BDWG 143A9481 REV -. PANEL LANDING FOUND TO HAVE 100% MATERIAL LOSS.SDR ASAA2025082960797Floorbeam · crackedAT PASSENGER CABIN CENTER WING STA.540 PANEL BREAK AT LBL-0 CRACKED (MARKED). GROUNDED - YES. PASSENGER CABIN CENTER WING STA 549 PANEL BREAK LBL-0 REMOVED AND REPLACED IAW B737-900 SRM 51-40-02-0G-0.SDR ASAA2025082761129Transition Panel · corrodedFWD CARGO TRANSITION PROFILE CORRODED AT STA 500L TO 500A AND BL 25R. GROUNDED - YES. REMOVED CORROSION AS REQ IN MULTIPLE AREAS. ORIG THICKNESS IS 0.040 PER SRM 53-30-53-01-02. LOWEST MATERIAL REMOVED WAS 0.020 REMAINING THICKNESS IS 0.020. FOUND TO BE OUT OFSDR ASAA2025082761128Shield · corrodedFWD CARGO TRANSITION PROFILE CORRODED AT BS 500 AND BL 25R. GROUNDED - YES. REMOVED FWD CARGO TRANSITION PROFILE AT STA 500. LOCATED AND DRILLED NEW PART IAW B737-900ER SRM 51-40-05. P/N 143A8126Y38 PO 1132983.1 PER B DWG 143A8126 REV -. INSTALLED NEW PART IN SDR ASAA2025082760554Transition Panel · corrodedFWD CARGO LH TRANSITION PANEL CORRODED AT STA 500H TO 500J. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS WITH 30% MATERIAL LOSS IAW B737-900ER SRM 53-30-53-01-2 AND 53-00-53-1A-2. TOOL T8224V CAL DUE 31/MAR/26. ACCOMPLISHED SIDEPLATE SPLICE SDR ASAA2025082661257Channel · corrodedAFT CARGO COMPARTMENT LONGITUDINAL FLOOR SUPPORT ASSEMBLY B/N: STA 727A & 727I, S-25L & S-26L, HAS MULTIPLE CORROSION SPOTS. GROUNDED - YES. DAMAGE FOUND TO BE CORRODED THROUGH IN MULTIPLE LOCATIONS WITH 100% MAT LOSS. FOUND TO BE OUT OF LIMITS IAW B737-900ER SDR ASAA2025082661255Channel · corrodedAFT CARGO COMPARTMENT LONGITUDINAL FLOOR SUPPORT ASSEMBLY BS 727A & 727I, S-25R & S-26R, HAS MULITPLE CORROSION SPOTS. GROUNDED - YES. DAMAGE FOUND TO BE CORRODED THROUGH IN MULTIPLE LOCATIONS WITH 100% MAT LOSS. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-01-2SDR ASAA2025082661090Floor Support · corrodedAFT CARGO COMPARTMENT LONGITUDINAL FLOOR SUPPORT ASSEMBLY B/N STA 727I & 767, S -25R & S -26R, HAS MULTIPLE CORROSION SPOTS. GROUNDED - YES. DAMAGE FOUND TO BE CORRODED THROUGH IN MULTIPLE LOCATIONS WITH 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS PER SRM 53SDR ASAA2025082660957Frame Splice · corrodedAFT CARGO COMPARTMENT RH LOWER FRAME B/N: STA 787, S-25R & S-24R HAS CORROSION. GROUNDED - YES. SPLICE HAS NO ALLOWABLE LIMITS REMOVED CORRODED SPLICE AND INSTALLED P#146A1300-3 PER B737-900ER SRM 51-40-02 AND BDWG 146A1262 REV J.SDR ASAA2025082660939Shield · corrodedAFT CARGO COMPARTMENT LONGITUDINAL FLOOR SUPPORT ASSEMBLY BETWEEN: BS 767 & 787. S25R & S26R, HAS MULTIPLE CORROSION SPOTS. GROUNDED - YES. BLENDED AWAY CORROSION, ORIGINAL THICKNESS (SHIELD) .050 MAT LOSS .017, REMAINING THICK .033, AREA OUT OF LIMITS PER SRMSDR ASAA2025082660849Web · corrodedFWD CARGO DOOR SCUFF PLATE SUB-STRUCTURE HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT CARGO DOOR LOWER WEB IAW SRM 53-30-15-1A-1 ORIGNAL MATERIAL THICKNESS IS 0.050 IAW SRM 53-30-15-01-1, REMOVED 0.020, REMAINING THICKNESSDR ASAA2025082660553Floor Support · corrodedAFT CARGO COMPARTMENT LONGITUDINAL FLOOR SUPPORT ASSEMBLY B/N STA 727I AND 847, S-25L & S-26L HAS MULTIPLE CORROSION SPOTS. GROUNDED - YES. DAMAGE FOUND TO BE CORRODED THROUGH WITH 100 PERCENT MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-60-53-SDR ASAA2025082560923Support · corrodedFWD CARGO COMPARTMENT AFT LEFT BULKHEAD SUPPORT STRUCTURE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT AFT L/H SIDE BULKHEAD SUPPORT IAW B737-900 SRM 53-30-08-1A-1, 100% MATERIAL LOSS AND FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-30-08-1A-SDR ASAA2025082260940Web · corrodedFWD CARGO DOOR WEB IS CORRODED IN NUMEROUS PLACES. GROUNDED - YES. CORROSION REMOVED, ORIGINAL THICKNESS .045, MAT LOSS .0175, REMAINING THICKNESS .0275, AREA OUT OF LIMITS PER B737-900ER SRM 53-30-15-1A-1 REMOVED WEB AND INSTALLED IAW SRM 51-40-02 AND DWG 143SDR ASAA2025082060778Floorbeam · corrodedSTA 947 FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION BETWEEN LBL-26 TO RBL-26. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REPAIRED IAW B737-900 SRM 53-70-51-2R-5W: 1" O: .150 R: 0 L: 1" D: .150.SDR ASAA2025082060624Floorbeam · corrodedCABIN FWD FLOOR WET AREA APPROX.STA.297 RBL 12, FLOORBEAM UPPER SURFACE CORRODED AROUND FASTENER HOLE (1EA). GROUNDED - YES. REMOVED CORROSION, ORIG THICK .080", REMOVED .033", REMAINING .047" FOUND OUT OF LIMITS IAW SRM 53-10-51, REMOVED AND REPLACED PANEL BSDR ASAA2025082060543Structure · corrodedR/H INNER CHORD CORRODED BETWEEN STA 1006 TO STA 1016. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-70-51-1A-1. REMOVED AND REPLACED INNER CHORD IAW B737-900 SRM 51-40-02-0G-0. W= 2.00 O= .080 R= .058 L= 2.00 D= .022.SDR ASAA2025081960250Handle · unsecureFLIGHT ATTENDANT REPORTS THAT DOOR L-2 SECURING LEVER WAS MOVING IN FLIGHT UPWARDS BETWEEN 1 TO 2 INCH AND SHE WOULD APPLY DOWNWARD PRESSURE TO THE LEVER BUT IT WOULD NOT STAY SECURED AT ITS BOTTOM RETENT. ADDITIONALLY SHE MENTIONED THAT THE CATERS HAD DIFFICUSDR ASAA2025081960222Elec Connector · damagedWIRE HANGING FROM CEILING OF AFT CABIN. GROUNDED - YES. REVERSED SP NR 2 MAINT. PROCEDURES- INSPECTED CONN'S AND FOUND NO ISSUES. REF SWPM 20-63-02. FULLY ATTACHED BOTH CONNECTOR HALVES AND VERIFIED LOCKED TOGETHER.EMERGENCY LIGHT NOW OPS NORMAL. REF MM 33-SDR ASAA2025081760297Battery Pack · inoperativeEMERGECNY LIGHTS ASSOCIATED WITH POWER SUPPLY M1694 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1694 AND TEST PASSED AIW B737-900 AMM 33-51-06-960-805.SDR ASAA2025081760296Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1695 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1695 AND TEST PASSEDD IAW B737-900 AMM 33-61-06-960-805.SDR ASAA2025081760295Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1676 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1676 AND TEST PASSED IAW B737-900 AMM 33-51-06-960-805.SDR ASAA2025081760294Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1671 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1671 AND TEST PASSED IAW B737-900 AMM 33-51-06-960-805.SDR ASAA2025081760293Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1670 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1670 AND TEST PASSED IAW B737-900 AMM 33-51-06-960-805.SDR ASAA2025081560626Frame · corrodedAFT CARGO FRAME BS 747 CORRODED AT INNER CHORD RBL 26. GROUNDED - YES. UPON FURTHER EVALUATION FOUND TO HAVE NO ALLOWABLE SRM LIMITS, REPAIRED FRAME BS 747 RBL 26 IAW SRM 53-60-07-2R-2W =1" O= .000 R= .000 L= 2" D= .000.SDR ASAA2025081560416Angle · corrodedAFT CARGO CORROSION ON ANGLE AT STA 767 TO 787 RBL 28. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 51-10-02. REMOVED AND REPLACED ANGLE ASSY IAW B737-900 SRM 51-40-02-0G-0.W= 1.00 O= .080 R= .038 L= 22.0 D= .042.SDR ASAA2025081360447Floor Panel · damagedAFT WET AREA FWD CENTER FLOOR PANEL IS DAMAGED. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF AFT WET AREA FWD CENTER FLOOR PANEL IAW SRM-53-00-50-2R-6.SDR ASAA2025081360078Lens · missingR1 DOOR EXIT SIGN COVER MISSING. GROUNDED - YES. INSTALLED NEW R1 DOOR EXIT LENS. PER AMM 33-51-01 OPS CHECK GOOD. NO DISCREPANCIES NOTED.SDR ASAA2025081260556Web · corrodedFWD CARGO DOOR SCUFF PLATE SUB FRAME HAS CORROSION IN MULTIPLE LOCATION. GROUNDED - YES. REMOVED CORROSION ON FWD CARGO THRESHOLD WEB ORIGINAL THICKNESS .045, REMOVED .012, REMAINING .033, FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-30-15. REMOVED DAMAGE WSDR ASAA2025081260448Transition Panel · corrodedAFT CARGO COMPARTMENT LT FLOOR TRANSITION PANEL, BS 727I+9 TO TO 847, LBL.21. UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-SDR ASAA2025081260446Transition Panel · corrodedAFT CARGO COMPARTMENT, RT FLOOR TRANSITION PANEL TO BS 727 TO 727I+9, RBL21, UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00SDR ASAA2025081260445Transition Panel · corrodedAFT CARGO COMPARTMENT LT FLOOR TRANSITION PANEL TO BS 727 TO 727I+9, LBL21 UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMIANING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-SDR ASAA2025081260444Transition Panel · corrodedAFT CARGO COMPARTMENT RT FLOOR TRANSITION PANEL BS 7271+9 TO BS 767, RBL21 UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1SDR ASAA2025081260443Threshold Web · corrodedAFT CARGO HAS CORROSION AT DOOR THRESHOLD. GROUNDED - YES. REMOVED CORROSION ON AFT CARGO DOOR THRESHOLD WEB ORIGINAL MAT. THICKNESS .050, MATERIAL REMOVED .026 MATERIAL REMAINING .024. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. REPLACED AFT CARGO THRESHOLD SDR ASAA2025081260379Shield · corrodedAFT CARGO COMPARTMENT R/H FLOOR SHIELD BS.767 TO BS.787+6 RBL.21 UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. EVALUATED R/H SHIELD STA 767 TO STA 787, ORIGINAL THICKNESS .050 REMOVED .010 REMAINING .040 FOUND TO BE OUT OF LIMITS IAW B737-900SDR ASAA2025081526044Lens · detachedEXIT SIGN CAME OFF AT ROW 16D. GROUNDED - YES. REPLACED LENS IAW AMM 33-51-01, NO OTHER DEFECTS NOTED.SDR ASAA2025081260043Cover · missingEXIT LIGHT COVER MISSING ROW 16 EXIT ROW A/C LEFT. GROUNDED - YES. REMOVED AND REPLACED EXIT FLOOR LIGHT ASSY AT ROW 16 ABC. OPS CHECK GOOD. REF AMM 33-51-01-960-802.SDR ASAA2025080960643Web · corrodedAFT CARGO DOOR CUTOUT LOWER SILL WEB CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAWRM 53-60-15-1A-1. REMOVED AND REPLACED SILL WEB IAW B737-900 SRM 51-40-02-0G-0W= 1.25 O= .050 R= .040 L= 2.25 D= .010.SDR ASAA2025080960545Shield · corrodedAFT CARGO FWD SHIELD CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-2. REMOVED AND REPLACED SHIELD IAW B737-900 SRM 51-40-02-0G-0. W= 1.25 O= .050 R= .010 L= 2.25 D= .040.SDR ASAA2025080960781Transition Panel · corrodedFWD CARGO L/H TRANSITION F.S. 500A-500C+10 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2, REPAIRED TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-6W- .50 O- .040 R- 0.0 L- 3.60 D- .040.SDR ASAA2025080960644Web · corrodedAFT CARGO DOOR CUTOUT LOWER SILL WEB CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED SILL WEB IAW SRM 51-40-02-0G-0W= 1.25 O= .050 R= .040 L= 2.25 D= .010.SDR ASAA2025080960638Cargo Track · crackedAFT CARGO RBL14 CARGO TRACK CRACKED AT BS 727I AND 727J. GROUNDED - YES. REMOVED DAMAGE, AND REREPAIRED CARGO TRACK IAW SRM 53-00-53-2R-3.SDR ASAA2025080960637Transition Panel · corrodedAFT CARGO RT TRANSITION BS 727I+10 - 767 CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIRED TRANSITION IAW SRM 53-00-53-2R-5W= 1.25 O= .040 R= .000 L= 4.50 D= .040.SDR ASAA2025080960635Transition Panel · corrodedAFT CARGO RT TRANSITION F.S. 727+4 - 727I+10 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, REPAIRED TRANSITION IAW SRM 53-00-53-2R-5W 2" O .040 R .000 L 2" D .040.
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