Boeing 737-990ER
Service difficulty reports · 10,341
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 ASAA2024112454673Angle · corrodedFWD CARGO COMPT STA 500L, LOWER BULKHEAD ATTACH ANGLE CORRODED. S 25R - S 25L. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT LOWER BULKHEAD ANGLE AT STA 500L IAW B737-900ER SRM 53-30-08-1A-1. MINIMUM ALLOWABLE REMAINING THICKNESS IS .056". REMAINING THICKNESSSDR ASAA2024112454533Bracket · crackedFWD CARGO COMPT. STA 500J RBL25, FRAME TO WEB BRACKET CRACKED. GROUNDED - YES. REMOVED DAMAGE BRACKET FROM FWD PIT STA. 500J, RBL25 IAW B737-900 SRM 51-40-02. LOCATED & DRILLED NEW BRACKET P/N: 143A7502U160, PO: 1108116.2 IAW B737-900 SRM 51-40-05, INSTALLED NSDR ASAA2024112454531Bracket · corrodedFWD CARGO COMPT, STA 500I RBL25, FRAME TO WEB BRACKET HAS SMALL AREA OF CORROSION. GROUNDED - YES. UPON FURTHER EVALUATION FRAME TO THE WEB BRACKET WAS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN THE B737-900 SRM, REMOVED DAMAGE BRACKESDR ASAA2024112454469Stringer Clip · crackedFWD CARGO COMPT, STA 500L FRAME TO S25R ATTACH BRACKET CRACKED. GROUNDED - YES. REMOVED R/H TRANSITION PANEL FROM STA 500H TO STA 500L FOR ACCES IAW B737-900 SRM 51-40-02 REMOVED ATTACH BRACKET AT STA 500L, STR25R IAW B737-900 SRM 51-40-02. LOCATED & DRILLED NSDR ASAA2024112454467Transition Panel · corrodedAFT CARGO, R/H TRANSITION PANEL HAS CORROSION FROM STA 727C TO 727I. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL FROM STA 727C TO 727I IAW B737-900ER SRM 53-00-53-1A-2. ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-60-53-01-1. REMOVED .SDR ASAA2024112454422Transition Panel · corrodedAFT CARGO, L/H TRANSITION PANEL HAS CORROSION FROM STA 727C TO 727I. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727C TO STA 727I IAW B737-900ER SRM 53-00-53-1A-2.2.D. 100% MATERIAL LOSS AND IS FOUND TO BE OUT OF LIMITS PER B737-SDR ASAA2024112454350Transition Panel · corrodedAFT CARGO, R/H TRANSITION PANEL HAS CORROSION FROM STA 727I TO 747. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL FROM STA 727I TO 747 IAW B737-900ER SRM 53-00-53-1A-2. ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-60-53-01-2. REMOVED .01SDR ASAA2024112454307Floorbeam · damagedMAIN CABIN FLOOR BEAM STA 440 AT 0 BUTLINE HOLE BE FOUND ENLONGATED. GROUNDED - YES. CUT OUT DAMAGE IAW B737-900ER SRM 53-00-51-2R-1. FABRICATED REPAIR ANGLES, FILLER AND SHIMS IAW B737-900ER SRM 53-00-51-2R-1. ALODINED IAW B737-900ER SRM 51-20-01. PRIMED IAW SDR ASAA2024112454303Angle · corrodedFWD CARGO COMPT, STA 500L, R/H LOWER BULKHEAD ATTACH ANGLE CORRODED, S 23R- S 25R. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT LOWER R/H BULKHEAD ANGLE AT STA 500L IAW B737-900ER SRM 53-30-08-1A-1. MINIMUM ALLOWABLE REMAINING THICKNESS IS .056" IAW B737-900SDR ASAA2024112355096Scuff Plate · corrodedAFT R2 DOOR AT SCUFF PLATE LANDING HAS CORRROSION IN SEVERAL PLACES GROUNDED - YES. REMOVED CORROSION IAW B737-900ER SRM 53-70-15-1A-1. ORIG MAT .080 REMAINING MAT AT LOWEST AREA IS .067 . MAT LOSS OF .013 IS BEYOND ALLOAWABLE LIMITS. REPAIRED AREA IAW ALASKA SDR ASAA2024112354545Floor Support · corrodedMAIN CABIN R2 DOOR LOWER SILL AREA PANEL SUPPORT HAS CORROSION AT BS960 AS MARK. GROUNDED - YES. REMOVED DAMAGE PER B737-900ER SRM 51-10-02, ORIGINAL THICKNESS .080, MAT REMOVED .030 MAT REMAINING .050 FOUND OUT OF LIMITS PER B737-900ER SRM 53-70-51-1A-1, REMOSDR ASAA2024112354057Battery Pack · inoperativeFOUND L1,L2,R1 & R/H OVERWING EMG. EXIT LTS INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK FOR R1 DOOR AND RH OVERWING EMERGENCY LIGHTS POWER SUPPLY REF AMM 33-51-06. REMOVED AND REPLACED BATTERY PACK FOR L1 & R2 DOOR (M1673) AND (M1675) OPS CHECK GOOSDR ASAA2024112154543Transition Panel · corrodedGENERATED FROM CUST CARD G2069500 TO REPAIR FWD PIT L/H TRANSITION PANEL FROM STA 500B TO 500L. GROUNDED - YES. REPAIRED FWD PIT L/H TRANSITION PANEL FROM STA 500B TO 500L IAW ASA B737-900 SRM 53-00-53-2R-5.SDR ASAA2024112154178Snubber · malfunctionedL2 DOOR HARD TO OPEN(PRI 2). GROUNDED - YES. (RESOLVED ON W/O: 2026596 TASKCARD: N/R-00003 ) DISCOVERED THE L2 DOOR SNUBBER WILL JAM AGAINST THE LOWER HINGE ARM WHEN OPENING DOOR FROM THE OUTSIDE. ADJUSTED GUIDE ARM RIG FOR GREATER CLEARANCES. NO FIX RETURNED SDR ASAA2024112154058Sign · inoperativeTHE "EXIT" SIGN NEAR THE L2 DOOR NEEDS REPAIR. GROUNDED - YES. REMOVED & REPLACED EXIT SIGN AT L2 DOOR. IAW 33-51-01-960-802. OPS CK NORMAL . THIS CLEARS PLT/ EA 900ER-33EA-27892SDR ASAA2024112154044Door · lack of lubeL2 DOOR WILL NOT OPEN. GROUNDED - YES. LUBED AND INSPECTED- AFT L2 DOOR. DOOR OPENS WITH NO FURTHER FAULTS AT THIS TIME AMM 52-13-51-200-801.SDR ASAA2024112154022Power Supply · inoperativeLEFT OVERWING EXIT LIGHTS ARE INOP. GROUNDED - YES. REMOVED AND REPLACED M1670 POWER SUPPLY IAW B737-900 AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2024112054544Floorbeam · corrodedCABIN FLOOR PANEL SUPPORT ANGLE CORRODED AT FASTENERS 4EA BS 867 RBL 63. GROUNDED - YES. ACCOMPLISHED REPAIR TO R/H CREASE BEAM IAW ALASKA EA#900ER-53EA-27932 DATED 12/12/2024. THIS IS A CATEGORY "A" REPAIR.SDR ASAA2024112054299Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-769 HAS PEELING FIBERS (PARTS RACK). GROUNDED - YES. CLEANED, SANDED, EVALUATED & REMOVED DAMAGE ON CABIN FWD WET AREA FLOOR PANEL 141A5810-769 AND REPAIRED IAW B737-900ER SRM 53-00-50-2R.SDR ASAA2024112054144Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-160 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON CABIN FLOOR PANEL 141A5810-160 FACESHEET IAW B737 SRM 53-00-50-2R-0.SDR ASAA2024112054143Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-768 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON CABIN FLOOR PANEL 141A5810-768 FACE SHEET IAW B737 SRM 53-00-50-2R-0.SDR ASAA2024112054141Floor Panel · damagedCABIN AFT WET AREA FLOOR PANEL 147A5800-440 HAS DELAMINATION & CORRODED INSERTS. (PARTS RACK). GROUNDED - YES. REPAIRED CABIN AFT WET AREA FLOOR PANEL 147A5800-440 IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR ASAA2024112054140Floor Panel · peelingCABIN AFT WET AREA FLOOR PANEL 147A5800-443, HAS DELAMINATION PEELING & CORRODED INSERTS. (PARTS PACK). GROUNDED - YES. REPAIRED CABIN AFT WET AREA FLOOR PANEL 147A5800-443 IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR ASAA2024112054139Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-454 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. PREFORMED PERMANT REPAIR TO CABIN FWD WET AREA FLOOR PANEL 141A5800-454 PEELING FIBERS IAW B737-900ER SRM 53-00-50.SDR ASAA2024112054138Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-155 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. PERFORMED PERMANT REPAIR TO CABIN FWD WET AREA FLOOR PANEL 141A5800-155 PEELING FIBERS IAW B737-900ER SRM 53-00-50.SDR ASAA2024112054137Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-735 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO CABIN FWD WET AREA FLOOR PANEL 141A5810-735 IAW ASA B737 SRM 53-00-50-2R-1.SDR ASAA2024112054136Floor Panel · peelingCABIN FWD WET AREA FLOOR PANEL 141A5800-736 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO CABIN FWD WET AREA FLOOR PANEL 141A5810-736 IAW ASA B737 SRM 53-00-50-2R-1.SDR ASAA2024112054118Floor Panel · damagedCABIN AFT WET AREA FLOOR PANEL 147A5800-398 HAS PEELING & CORRODED INSERTS. (PARTS RACK). GROUNDED - YES. REPAIRED CABIN AFT WET AREA FLOOR PANEL 147A5800-398 IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR ASAA2024112054117Floor Panel · damagedCABIN AFT WET AREA FLOOR PANEL 147A5800-444, HAS DELAMINATION PEELING & CORRODED INSERTS. (PARTS RACK). GROUNDED - YES. CLEANED, EVALUATED & REMOVED DAMAGE ON CABIN AFT WET FLOOR PANEL 147A5800-444 AND REPAIRED IAW B737-900ER SRM 53-00-50-2R & 51-SDR ASAA2024112054116Floor Panel · damagedCABIN AFT WET AREA FLOOR PANEL 147A5800-439 HAS PEELING FIBERS & CORRODED INSERTS. (PARTS RACK). GROUNDED - YES. CLEANED,EVALUATED & REMOVED DAMAGE ON CABIN AFT WET AREA FLOOR PANEL 147A5800-439 AND REPAIRED IAW B737-900ER SRM 53-00-50-2R & 51-40-02.SDR ASAA2024112054115Floor Panel · damagedCABIN AFT WET AREA FLOOR PANEL 147A5800-445 HAS PEELING FIBERS & CORRODED INSERTS. (PARTS RACK). GROUNDED - YES. PREFORMED PERMANT REPAIR TO CABIN AFT WET AREA FLOOR PANEL 147A5800-445 DELAMANTED FIBERS IAW B737-900ER SRM 53-00-50.SDR ASAA2024112054114Floor Panel · damagedCABIN FWD WET AREA FLOOR PANEL 141A5800-738 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. REPAIRED CABIN FWD WET AREA FLOOR PANEL 141A5800-738 IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR ASAA2024112054113Floor Panel · damagedCABIN FWD WET AREA FLOOR PANEL 141A5800-739 HAS PEELING FIBERS. (PARTS RACK). GROUNDED - YES. REPAIRED CABIN FWD WET AREA FLOOR PANEL 141A5800-739 IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-1, AND SRM 53-00-50-2R-0.SDR ASAA2024111954542Transition Panel · corrodedFWD CARGO COMPARTMENT RH TRANSITION PANELS HAVE CORROSION AREAS MARKED WITH RED. GROUNDED - YES. EVALUATED DAMAGE/CORROSION FROM FWD PIT R/H TRANSITION PANEL FROM STA 500A-STA 500L IAW B737-900ER SRM 53-00-53-1A-2. ORIG THICKNESS : .040 IAW B737-900ER SRM 53-6SDR ASAA2024111954496Web · corrodedFWD CARGO COMPARTMENT AT CUTOUT LOWER SILL WEB HAS CORROSION. GROUNDED - YES. EVALUATED FWD PIT DOOR WEB IAW B737-900ER SRM 53-30-15-1A-1. ORIG THICKNESS IS ..045 IAW B737-900ER SRM 53-30-15-0I-1. REMOVED: .015 REMAINING: .030 AND IS FOUND TO BE OUT OF LIMITS SDR ASAA2024111953979Lens · detachedF/A ADVISED ROW 16A OVERWING EXIT SIGN COVER FELL OFF. THIS SIGN IS LOCATED JUST BELOW AND TO THE RIGHT OF THE OVERWING EXIT. GROUNDED - YES. INSTALLED ROW 16A OVERWING EXIT SIGN COVER LOCATED JUST BELOW AND TO THE RIGHT OF THE OVERWING EXIT PER ASA B737-900ERSDR ASAA2024111854702Web · corrodedAFT CARGO THRESHOLD WEB HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM WEB SILL. ORIGINAL THICKNESS .045 IAW B737-900 SRM 53-60-15-0I-1. MATERIAL LOSS OF .009. REMAINING IS .036. OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-1. REMOVED & REPLACED WEB SILL SDR ASAA2024111854596Shield · corrodedAFT CARGO R/H FWD SHEILD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM SHEILD ORIGINAL THICKNESS .050 IAW B737-900ER SRM 53-60-15-01-1 MATERIAL LOSSED .007 REMAINING THICKNESS .043 FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-60-15-1A-1 TOOL#T8224V SDR ASAA2024111854541Transition Panel · corrodedAFT CARGO L/H TRANSITION PANEL HAS CORROSION FROM FWD BULKHEAD TO 727E. GROUNDED - YES. REMOVED CORR. FROM AFT CARGO L/H TRANSITION PNL FROM FWD BULKHEAD TO STA 727E I.A.W B737-900 SRM 53-00-53. ORIG. THICKNESS .040 I.A.W B737-900 SRM 53-60-53 MAT. LOSSED .010SDR ASAA2024111854530Transition Panel · corrodedAFT CARGO L/H TRANSITION PANEL HAS CORROSION FROM STA 727I TO 847. GROUNDED - YES. REMOVED AND EVALUATED DAMAGE FROM AFT PIT L/H TRANSITION PANEL FROM STA727I-847 IAW B737-900ER SRM 53-00-53-1A-2. ORIG THICKNESS: .040 IAW B737-900ER SRM 53-60-53-0I-2. REMOVED SDR ASAA2024111854529Transition Panel · corrodedAFT CARGO R/H TRANSITION PANEL HAS CORROSION FROM STA 727E TO 727I. GROUNDED - YES. REMOVED CORR. FROM AFT CARGO R/H TRANSITION PANEL FROM STA.727E TO 727I I.A.W. B737-900 SRM 53-00-53. ORIG THICKNESS .040 I.A.W. B737-900 SRM 53-60-53. MAT. LOSSED .010 REMAINISDR ASAA2024111854528Transition Panel · corrodedAFT CARGO R/H TRANSITION PANEL HAS CORROSION FROM STA 727I TO 767. GROUNDED - YES. REMOVED CORR. FROM AFT CARGO RH TRANS. PNL STA 727I TO 767 I.A.W. B737-900 SRM 53-00-53. ORIG THICKNESS .040 I.A.W. B737-900 SRM 53-60-53. MAT LOSSED .010 REMAINING THICKNESS .0SDR ASAA2024111854498Transition Panel · corrodedAFT CARGO L/H TRANSITION PANEL HAS CORROSION STA 727E TO 727I. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT TRANSITION PANEL FROM STA 727E-727I IAW B737-900ER SRM 53-00-53-1A-2. ORIGINAL THICKNESS .040 IAW B737-900ER SRM 53-60-53-01.2 REMOVED .010 AND .030 RSDR ASAA2024111854497Cargo Track · corrodedAFT CARGO R/H FLOOR SUPPORT AT STA 767, 2ND SUPPORT ON RIGHT HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H FLOOR SUPPORT AT STA 767, RBL 13.84 IAW B737-900ER SRM 53-00-53-1A-2. ORIG. THICKNESS IS .070" IAW B737-900ER SRM 53-60-53-01-2 AND BSDR ASAA2024111854391Transition Panel · corrodedAFT CARGO R/H TRANSITION PANEL HAS CORROSION FROM FWD BULKHEAD TO 727E. GROUNDED - YES. EVALUATED AFT PIT R/H TRANSITION PANEL FROM STA 727A-STA727E IAW B737-900ER SRM 53-00-53-1A-2, ORIG THICKNESS: .040 IAW B737-900ER SRM 53-60-53-OI-2, REMOVED : .10 REMAININSDR ASAA2024111754295Floorbeam · corrodedAFT WET AREA 986.5 FLOOR BEAM HAS CORROSION AT LBL 40. GROUNDED - YES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 57-50-51-1A-1, ORIGINAL THICKNESS .150, MAT REMAINING .090 PER BAC DWG# 147A5506 REV-, CUT AND REMOVED DAMAGE PART OF FLOOR BSDR ASAA2024111754294Floorbeam · corrodedAFT WET AREA 986.5 FLOOR BEAM HAS CORROSION AT RBL 40. GROUNDED - YES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 57-50-51-1A-1 ORIGINAL THICKNESS .150, MAT REMAINING .085 PER BAC DWG# 147A5506 REV-, CUT AND REMOVED DAMAGE PART OF FLOOR BESDR ASAA2024111554258Web · corrodedAFT CARGO PIT THRESHOLD WEB HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT CARGO PIT THRESHOLD WEB. ORIG .050",REMOVED.007" REMAINING .043. FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-1. REMOVED WEB IAW B737-900 SRM 51-4SDR ASAA2024111554257Web · corrodedFWD CARGO PIT THRESHOLD WEB HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL MATERIAL THICK .045" REMOVED .009" REMAINING .036" FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-30-15-1A-1. LOCATED AND DRILLED NEW FWD CARGO DOOR THRESHSDR ASAA2024111453898Light · detachedEMERGENCY LIGHT ABOVE 27ABC POPPED OUT. GROUNDED - YES. REINSTALLED EMERGENCY AISLE LIGHT ABOVE SEAT 27ABC, OPS CHECK NORMAL PER AMM 33-51-03.
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