Boeing 737-83N
Service difficulty reports · 1,087
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 = '73783N' 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 = '73783N' 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 SCNA20240309071Stiffener · crackedUPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE AREA AT BODY STATION 540 CENTER FUEL TANK STIFFENERS WITH CRACK AT FOLLOWING POSITIONS. RBL AND LBL7, 15, 32, 41 AND 53. REPLACED STIFFENERS P/N: 111A2401-1 (5EA) AND P/N: 111A2401-2 I-A-W B-737-800 BCF S-R-M SDR SCNA20240309073Pressure Deck · corrodedLOWER FUSELAGE RIGHT MAIN WHEEL WELL PRESSURE FLOOR STRUCTURE WITH CORROSION ARROUND GROUND STUD #G310DC LOCTED AT BS 717 RBL 30. PERFORMED PERMANENT REPAIR AT SPANWISE STIFFENER, PRESSURE FLOOR STA 716 AT RBL 30 IAW COOPESA E.0 # COO-EO-2024-19510-ROO DATEDSDR SCNA20240309072Bulkhead Web · crackedLOWER FUSELAGE MAIN WHEEL WELL RIGHT SIDE, FWD BULKHEAD LOWER WEB WITH CRACK AT RBL 9. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE MAIN W/W R/H SIDE FWD BULKHEAD LOWER WEB AT RBL 9 IAW B737-800 BCF SRM TASK 57-10-10-1A-2 A/D2 PARAGRAPH 2.C (4)(A)6)D) AND SRSDR SCNA20240309062Intercostal · crackedAFT CARGO COMPARTMENT FROM STA 827 TO STA 847 AT LBL20 INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL I-A-W BOEING SRM 51-10-02-0G-0 PARAG 9A.SDR SCNA20240118015Slide · dislodgedDEFECT 755160: - - DOOR 1L SLIDE FELL OUT OF THE DOOR. - - RESOLUTION: RE-INSTALLED L1 DOOR EVAC SLIDE PACK +COVERT IAW AMM 25-66-01 OK FOR SERVICE.SDR SCNA20240309070Shear Tie · crackedFWD CARGO COMPARTMENT AT STA 500I BETWEEN STR-25L STR-26L FRAME WITH CRACK. REPLACED (SHEAR TIE) P/N # 143A3010-69 FWD CARGO COMPARTMENT AT STA 500I BETWEEN STG 25R AT STG 26R I-A-W B-737-200-800 SRM 51-10-02-0G-0 PARAG 9SDR SCNA20240309061Stiffener · crackedREPLACED TOP STIFFENER P/N 111A2401-2 AND 111A2401-1 AT B%S 550 BETWEEN RBL 6" AND RBL 54" IAW B737-800 BFC SRM 51-10-02-0G-0 PARG 9 AND BOEING INST DWG 111A2000 SHEET 13 AND SHEET 14SDR SCNA20240308060Angle · crackedMAIN CARGO DECK FLOOR TRANSVERSAL ANGLE FLANGE IS CRACKED AT BS 540, RBL 24. EMP# 157 QC# 25 REPLACED BREAK IAW B737-800 BCF SRM 51-10-02-0G-0 PARG 9 AND BOEING INST. DWG 143A0060 SHEET 2 REV BSDR SCNA20240308059Spar Web · corrodedEMP# 157 QC# 25 RII# QC25 PERFORMED PERMANENT REPAIR OF RH WING FRONT SPAR WEB AT FWD FUEL BOOST PUMP DUE TO CORROSION OUT LIMITS IAW COOPESA EO# 600-EO-2024-19231-R00 DATED: 01/171/2024 DOCUMENTED ON FAA FORM 8100-9 REFERENCE ID: 202401160018-003. THIS REPAISDR SCNA20240129021Window · crackedDEFECT 752097: - - R1 OVERHEAT FOLLOWED BY SPIDER CRACK ON OUTER PANE OF R1. - - RESOLUTION: (TRANSFERED LOG ITEM 752097 ITEM 1 TO W/O# 84410 N/R 00003) REMOVED R1 WINDOW REF AMM 56-11-11, BEGAN TO INSTALL NEW WINDOW, DONE THRU STEP 6 REF AMM 56-11-11. FINISHSDR SCNA20240311149Bulkhead · crackedAFT CARGO COMPARTMENT, FWD BULKHEAD PANELS: 141JW, 142MW WITH CRACKS. BULKHEAD PANELS DAMAGE WERE FOUND GREATER THAN THE LIMITS I.A.W BOEING 737-800 AMM SCA TASK 25-52-00-200-806 PARAGRAPH 6.D(5) REV 82 DATED 10-15-2023 REPLACED AFT CARGO COMPARTMENT, FWD BULSDR SCNA20240309066Bulkhead · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD AT 500I THE LEFT RAIL, CENTER RAIL AND RIGHT RAIL WITH CORROSION. REPLACED SUPPORT AND ANGLES P/N143A9495Y23, 143A9485-35 AND 143A9485-34 FWD CARGO COMPARTMENT AFT BULKHEAD AT STA 500I I-A-W B-737-800 SRM 51-10-02-0G-0 PARAGSDR SCNA20240309065Intercostal · crackedAFT CARGO COMPARTMENT FROM STA 747 TO STA 767 AT RBL20 INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL AFT CARGO COMPARTMENT FROM STA 747 TO STA 767 AT RBL 20 I.A.W BOEING 737-800 BCF SRM 51-10-02 PARAG 9.SDR SCNA20240309064Intercostal · crackedAFT CARGO COMPARTMENT FROM STA 727A TO STA 727B AT LBL20 AND RBL20 INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL IAW B-737-800 SRM 51-10-02-0G-0 PARAG 9SDR SCNA20240309063Cargo Track · crackedAFT CARGO COMPARTMENT FROM STA 787 TO STA 807 AT LBL 17.24 DOWN TRACK-TIE CARGO SECTION WITH CRACK. PERFORMED PERMANENT REPAIR AT CARGO TRACK SECTION FROM STA727D+3 TO STA 821 ON LBL 17.24 IAW B737-800 BCF-SRM-53-00-53-2R3-REPAIR 3 FIGURE 201.SDR SCNA20240309069Baffle · corrodedLOWER FUSELAGE, FWD CARGO COMPARTMENT. FROM STA 500H TO STA 500I AT RBL 21 AND LBL 21 THE INTERCOSTALS (BAFLES) WITH CORROSION. REPLACED (BAFLES) INTERCOSTALS FROM STA 500H TO 500I AT 21 RBL AND 21 LBL IAW B737-800 BCF SRM 51-40-02-0G-0 PARG 4B AND BOEING INSSDR SCNA20240309068Baffle · corrodedLOWER FUSELAGE, FWD CARGO COMPARTMENT. FROM STA 500A TO STA 500I AT RBL 21 THE INTERCOSTALS (BAFLES) WITH CORROSION. REPLACED (BAFLES) INTERCOSTALS FROM STA 500A TO STA 500I AT RBL 21 IAW B737-800 BCF SRM 51-10-02-0G-0 PARG 9 AND BOEING DWG 143A7505 REV BSDR SCNA20240309067Baffle · corrodedMRO ZONE 1 NR# 10 EMP# 6434 W/O:77911,TASK CARD #538200000:LOWER FUSELAGE, FWD CARGO COMPARTMENT. FROM STA 400 TO STA 500H AT LBL 21 THE INTERCOSTALS (BAFLES) WITH CORROSION. EMP# 157 QC# 25 REPLACED (BAFLES) INTERCOSTALS FROM STA 400 TO STA 500H LBL 21" IAW SDR SCNA20240305058Floor Support · corrodedAFTER GILL LINER REMOVAL IN LEFT BELLY AFT CARGO, CORROSION WAS FOUND ON FLOOR SUPPORT AT APPROX STA 792 TO STA 787. PER ENGINEERING, AFT CARGO DEPT SHALL REMAIN EMPTY, AFT CARGO FLOOR LINER REASSEMBLED, CARGO TAPE INSTALLED TO MAINTAIN SMOKE AND FIRE INTEGRISDR UIEA2023122001007Pump · unknownLEFT CENTER FUEL PUMP "LOW PRESSURE ILLUMINATED IN FLIGHT. RAN QRH ACCORDINGLY(<P>21DEC23 - 1699547 - ITEMS M1-M3- PDX - FOUND BOOST PUMP TANK CTR LEFT C/B TRIPPED UPON A/C RETURN. TROUBLESHOOT PER B737 FIM 28-22 FT 801. PER MCC DIRECTION, REPLACED R54 (BOOST SDR SCNA20230824209Unknown · unknownDEFECT 705338: DURING CRUISE L1 WINDOW STARTED ARCING AND CAUSED SEVERE DAMAGE TO OUTER PANE.- - - RESOLUTION: (IN PROGRESS)SDR SCNA20230815208Unknown · unknownDEFECT W/O 81151 NRC00002: #3 BRAKE WAS WRITTEN UP BY FLIGHT CREW AS READING 8.6 INSPECTION OF BRAKE FOUND IT GLOWING RED AND STARTED ON FIRE. - - - RESOLUTION: (IN PROGRESS)SDR UIEA2023063000673Doubler · unknownLOWER FUSELAGE, EXTERNAL POWER RECEPTACLE, INNER DOUBLER WITH CRACK.(<P>R/R INNER DOUBLER P/N: 141A3722-12 AT EXTERNAL POWER RECEPTABLE IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9 </P>)SDR UIEA2023063000674Unknown · unknownLH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 7 WITH CRACK (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-522)(<P>PERFORMED PERMANENT REPAIR ON REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN LBL 5 TO LBL 18.5 DUE TO CRACKS IAW B737-800 BCFSDR UIEA2023063000675Radio Altimeter · unknownNAVIGATION - RADIO ALTIMETER SYSTEM - INSTALLATION OF COLLINS LRA-900 LOW RANGE RADIO ALTIMETERS - STC ST02002WI - AD 2021-23-12 IAW ATLAS AIR EO 3834A029 REV.0, PARTS 1.(<P>PERFORMED NAVIGATION - RADIO ALTIMETER SYSTEM - INSTALLATION OF COLLINS LRA-900 LOW RASDR UIEA2023063000676Unknown · unknownFUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - POST PREVENTIVE MODIFICATION INSPECTION - SB 737-53-1335 - AD 2013-19-23 AMOC IAW ATLAS AIR EO 3853A035 REV.0, PARTS 2-3.(<P>PEFORMED POST PREVENTIVE MODIFICATION INSPECTION - SB 737-53-1335 - AD 2SDR UIEA2023072800763Unknown · unknownRT WING FUEL TANK STIFFENER WITH CRACK, BETWEEN RIB 21 & RIB 22 (OBSERVED WHILE PERFORMING THE 20 YEARS INSPECTION)(<P>PERFORMED PERMANENT REPAIR ON RH OUTBOARD WING UPPER STRINGER U-9 DUE TO CRACK IAW COOPESA EO #: COO-EO-17861-R01 (JUL/15/23) DOCUMENTED AND SDR 2023F00250Module · failedENGINE #1 OVERHEAT DURING CLIMB PHASE. CORRECTIVE ACTION: CHANGED OVERHEAT DETECTION CONTROL IAW AMM 26-18-01/401 AND TEST OK.SDR SCNA20230828211Unknown · unknownDEFECT 746816: RH FWD EMERGENCY EXIT OVERWING DOOR EMERGENCY LIGHT INOP ( EXTERIOR EMERGENCY LIGHTING SYSTEM ) - - - RESOLUTION: REMOVED AND REPLACED R2 EMERLIGHT CHARGE ASSY REF AMM 33-51-00 OPS CHECK GOOD THIS CLEARS MEL 33-14 MDDR#8311MSDR SCNA20230619189Unknown · unknownDEFECT 724361: R1 AND R2 EMERGENCY LIGHT BATTERIES ARE BAD. - - - RESOLUTION: (IN PROGRESS)SDR UIEA2023052500522Unknown · unknownPAX CABIN FWD ENTRY AREA WL 208.1 AT LBL 60, BETWEEN BS 332.1 AND BS 294.5 SIDE BEAM WITH CRACK.(<P>PERFORMED PERMANENT REPAIR ON LOWER MAIN SILL INNER CHORD FWD ENTRY AREA AT BWL 208.1, LBL 60 AT BS 303.9 DUE TO CRACK I/A/W COOPESA E.O #COO-EO-2023-17712-R00 SDR UIEA2023052500523Unknown · unknownWHILE PERFORMING AFT BULKHEAD INSPECTION WAS FOUND PERMANENT REPAIR LOCATED BETWEEN B/S 1016 & B/S 1046, BETWEEN STR 13L & STR 16L WITH LIGHT CORROSION(<P>PERFORMED PERMANENT REPAIR FUSELAGE SKIN SECTION FROM BS 1016 TO BS 1040 BETWEEN STR 13L AND STR 16L. DUESDR UIEA2023053000530Unknown · unknownDURING PAINT REMOVAL PROCESS FOR N.D.T. INSPECTION, WAS FOUND FASTENERS HEADS WITH CORROSION ON R/H WING, REAR SPAR UPPER CHORD FROM RIB 5 TO RIB 14,(<P>REMOVED CORROSION I/A/W B737-800 BCF SRM 51-10-02-0G-0 PARAG 15A AND EVALUATED REWORK AREA AND FOUND IT WISDR UIEA2023053000531Unknown · unknownLOWER FUSELAGE FWD CARGO COMPARMENT DOOR EXTERNAL SKIN SECTION AT BSTA 457 BETWEEN BEAM B AND BEAM C; BSTA 470 BETWEEN BEAM B AND BEAM C; BSTA 474 BETWEEN BEAM D AND BEAM E AND BSTA 485 BETWEEN BEAM B AND BEAM C SKIN WITH DENTS.(<P>PERFORMED PERMANENT REPAIR ASDR UIEA2023053000532Unknown · unknownFAA FINDING AFT CARGO COMPARTMENT STR 25LH EVIDENCE OF CORROSION ON ENTIRE LENGTH OF FLOOR CHANNEL SUPPORT(<P>EVALUATED REWORKED AREA AS FOUND WITHIN ALLOWABLE DAMAGE LIMITS I/A/W B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAG 4A(2) FIG 103 DETAIL D, ORIGSDR UIEA2023053000533Unknown · unknownLT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT LBL 41 WITH CRACK. (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-549)(<P>PERFORMED PERMANENT REPAIR AT LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM LBL 5 TO LBL 41, DUE TO CRSDR UIEA2023053000534Unknown · unknownLT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT LBL 6 WITH CRACK. (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-549)(<P ><SPAN LANG="EN-US">PERFORMED PERMANENT REPAIR AT LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM LBL 5 TSDR UIEA2023053000535Unknown · unknownRT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 6 WITH CRACK.( FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-550)(<P><SPAN LANG="EN-US">PERFORMED PERMANENT REPAIR AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 5 TOSDR UIEA2023053000536Unknown · unknownRT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 41 WITH CRACK.( FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-550)(<P ><SPAN LANG="EN-US">PERFORMED PERMANENT REPAIR AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 5 SDR UIEA2023053000537Unknown · unknownDURING PAINT REMOVAL PROCESS FOR N.D.T. INSPECTION, WAS FOUND FASTENERS HEADS WITH CORROSION ON L/H WING, REAR SPAR UPPER CHORD FROM RIB 5 TO RIB 14.(<P>REMOVED CORROSION I/A/W B737-800 BCF SRM 51-10-02-0G-0 PARAG 15A. EVALUATED REWORKED AREA AND FOUND IT WITHSDR UIEA2023053000538Unknown · unknownPAX CABIN FWD ENTRY AREA, RH SIDE BEAM WITH CORROSION BETWEEN BS 303.9 AND BS 344 WL 208.1 RBL 60.(<P>REMOVED CORROSION AT R/H SIDE BEAM (INNER CHORD) I/A/W B737-800 SRM 51-10-02-0G-0 PARAG 15A AND EVALUATION. REWORKED AREA AND IT WAS FOUND WITHIN ALLOWABLE DASDR UIEA2023053100545Doubler · unknownFUSELAGE - SECTION 41- RHS ELECTRICAL GROUND RECEPTACLE (EGPR) CUTOUT DOUBLER ( PN 141A3722-12) DEFORMATION - CATEGORY C TIME LIMITED REPAIR IAW ATLAS AIR EO 3853A157 REV.0, PARTS 2.(<P>REPLACED DOUBLER P/N: 141A3722-12 FUSELAGE SECTION 41 RHS ELECTRICAL GROUNSDR UIEA2023053100546Check Valve · unknownLEFT WING CENTER FUEL TANK, FOUND A FLAPPER VALVE WITH HALF THE LUGS BROKEN AT BOTTOM ROOT OF SKIN RIB 1.(<P>REPLACED REFUELING CHECK VALVE AT CENTER TANK, RH AND LH TANKS, I/A/W BOEING 737-800 AMM TASK 28-21-32-00-801 AND AMM TASK 28-21-32-400-801 PARAG 3 A TSDR UIEA2023053100547Antenna · unknownUPPER FUSELAGE, MAIN CARGO COMPARTMENT, DURING ELT SYSTEM TEST FOUND ELT UNIT SHOWING 3 FLASHES FAULT CODE.(<P>PERFORMED T/S AND FOUND ELT SYSTEM ANTENNA INTERNAL IMPEDANCE OUT OF RANGE AND ELT UNIT DISPLAYING INCORRECT A/C'S REGISTRATION NUMBER REPLACED AND TSDR UIEA2023053100548Unknown · unknownWHILE PERFORMING LH HORIZONTAL STAB. REAR SPAR LOWER LUG BUSHING REPLACEMENT WAS FOUND LOWER LUG AFT FACE WITH CORROSION(<P>REMOVED CORROSION FROM L/H HORIZONTAL STAB REAR SPAR LOWER LUG AFT FACE I/A/W S/B 737-55-1074 ISSUE R00 DATED 15-AUG-02 FIG 10 PART D SHSDR SCNA20230614185Unknown · unknownDEFECT W/O 74298 NR00029: DETERIORATED EMERGENCY LIGHT ON LH EMERGMENCY EXIT FWD. - - - RESOLUTION (IN PROGRESS)SDR 2023F00142Unknown · unknownL ENGINE BLEED TRIP OFF LIGHT ILLUMINATES WHEN SETTING TAKE OFF TRUST. CORRECTIVE ACTION: HAS BEEN PERFORMED FIM BLEED TRIP OFF LIGHT PROCEDURE IAW FIM 36-10 TASK 801 PART F PRELIMINARY CHECK AND ENGINE #1 RUN UP PERFORMED IAW AMM TASK 71-00-00-800-808 NO SHOWSDR 2023F00135Unknown · unknownDURING TAKEOFF BLEED TRIPOSS LIGHT ILLUMINATED BELOW 80 KNOTS. CORRECTIVE ACTION:BLEED TRIPOFF LIGHT PROCEDURE HAS BEEN PERFORMED IAW FIM 36-10 TASK 801 STEP F. PRELIMINARY CHECK AND ENGINE START NORMAL PROCEDURE PERFORMED IAW TASK 71-00-00-800-808 NOT TRIP OFSDR UIEA2023042000373Unknown · unknownLOWER FUSELAGE, AFT CARGO COMPARTMENT, AT BS 727G +18", LBL 21.5", ZEE CHANNEL WITH CRACK.(<P>REPAIRED SIDEPLATE SECTION AT LBL 21.5 BETWEEN BS727E+6.5" AND BS727J+16" I/A/W B737-800 BCF SRM 53-00-53-2R-6 REPAIR 6, PARAG 4 FIG 203</P>)SDR UIEA2023042000374Unknown · unknownLOWER FUSELAGE, FWD CARGO COMPARTMENT, AT BS 540, STGR 27L, STRINGER WITH CORROSION.(<P>REPAIRED FUSELAGE STRINGER 27LH BETWEEN BS500G+1.5" AND BS540 I/A/W B737 BCF SRM 53-00-03-2R-1 REPAIR 1 PARAG 4 FIG 205</P>)
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