Boeing 737-330
Service difficulty reports · 430
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 = '737330' 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 = '737330' 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 TSAA20211117051Stringer Clip · crackedREPLACED STRINGER CLIP STA 685 STR 10L IAW ALOHA AIR CARGO ECO 3759 REV 2 3/20/17 PARA 8.0 PART III FIGURE 16.SDR TSAA20211117023Intercostal · cracked1000582022 - REPLACED INTERCOSTAL AT STA 328, LBL 47 FWD GALLEY FLOOR STRUCTURE IAW BOEING DRAWING NUMBER 65-45834 REV HD, FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 PG 2 REV 125.SDR TSAA20211117052None · noneREPLACED AUXILIARY CHORD AT STA 727 LH BETWEEN STR 17L & STR 22L. I.A.W. B737-300 SRM REV 126 CH 51-40-02 REF BOEING DOC #65-46547 REV:DK.SDR TSAA20211117053Beltframe · crackedREPLACED BELTFRAME @ FS 440 R/H SIDE BETWEEN ST 17R-16R WITH MADE REPAIR PART IAW B737-300 SRM REV 125 51-10-02 PARA 8. INSTALLED BELTFRAME IAW BOEING DWG 65-20722 REV: AH AND
B737-300 SRM REV 125 51-40-02.SDR TSAA20211117022Bulkhead Web · cracked1000581539 - REPAIRED CRACK EMANATING FROM FASTENER ON STA 1016 BULKHEAD AT CABIN FLOOR LEVEL AT LBL9 AFT FACE OF BULKHEAD IAW KF AEROSPACE DRAWING #R27904.1-53-018-001 REV NC.SDR TSAA20211117021Antenna · cracked1000580928 - CRACKS FOUND (X4) COMMON TO THE FOOTPRINT OF THE #3 VHF ANTENNA REPAIR REMOVED IAW SB737-53-1287 REV 1 NOVE 15, 2010 AND REPAIRED IAW DWG NO.R27904.1-053-021-001 REV NC.SDR TSAA20211117055Pitot System · noneCOMPLIED WITH AD 2019-09-01. PERFORMED PITOT-STATIC MOD, TEMPERATURE PROBE AND ALPHA VANE ANTI-ICING SYSTEM TEST SERVICEABLE I.A.W. ALOHA AIR CARGO ECO 4233 PT.II, REV.1
DATE: 9/17/2021.SDR TSAA20211117056Stringer Splice · crackedCOMPLIED WITH AD 2014-01-05, PERFORMED INSPECTION OF STRINGER SPLICES AND BUTT STRAPS AND REPLACEMENT IAW ALOHA AIR CARGO ECO 3866, PT. II, REVISION 1, DATE: 8/17/17, CRACKS FOUND. SEE NDT REPORT NDT21-1540 ON STRINGER SPLICE AT STA 908 AT STR 4R & 4L CRACKS SDR TSAA20211117020Beltframe · dented1000578902 - DENT ON BELT FRAME STA 727B STR24R ASSESSED IAW B737-300 SRM REV 125 CH 53-00-07 FIG 101 SHEET 2 NOTE E AND FOUND TO BE BEYOND ALLOWABLE LIMITS. DENT IS ON THE FREE FLANGE AND NOTE
E STATES, "DENTS ALLOWED IN FRAME WEBS ONLY" REPLACED DENTED BELTSDR TSAA20211117019Beltframe · dented1000578901 - DENTS (X2) ON BELT FRAME STA 727C STR 23L-25L ASSESSED IAW B737-300 SRM REV 125 CH 53-00-07 FIG 101 SHEET 2 NOTE E AND FOUND TO BE BEYOND ALLOWABLE LIMITS. DENTS ARE ON THE FREE FLANGE. NOTE ESTATES "DENTS ARE ALLOWED, IN FRAME WEB ONLY". DENTED BSDR TSAA20211117057Anti-Ice System · failed inspCOMPLIED WITH AD 2019-09-01, INSTALL NEW J18 JUNCTION BOX TO CHANGE ANTI-ICING SYSTEM MOD, AND WIRING PROVISIONS TO ANTI-ICING SYSTEM IAW ALOHA AIR CARGO ECO 4233 PART 3, REV 1.SDR TSAA20211117018Beltframe · gouged1000575816 - DENT/ GOUGE ON BELT FRAME REPAIR MEMBER INNER FLANGE@ F.S. 500 RH SIDE BETWEEN STR 17R-16R BEYOND LIMITS AND REPLACED WITH NEW FABRICATED REPAIR MEMBER IAWAEI ENGINEERING ORDER # EO9520 REV IRSDR TSAA20211117017Angle · cracked1000575571 - CRACKED L-ANGLE ON FLOOR STRUCTURE AT FWD WET AREA STA 328, RBL 32, WL 200 REPLACED WITH MADE REPAIR PART FABRICATED AND INSTALLED I.AW B.737-300 SRM REV 125 CH 51-30-01 AND
51-40-02. REFERENCE BOEING DWG 65-45812 ID:0003 REV: LAND PL REV: CR FORSDR TSAA20211117016Anchor Fitting · cracked1000575570 - X2 CRACKED L-ANGLES FROM FRAMES TO WEB IN E&E BAY STA'S 320 AND 328 BETWEEN STR 20L AND 21L WERE REPLACED WITH MADE REPAIR PARTS FABRICATED AND INSTALLED I.AW B.737-300 SRM
REV 125 CH 51-30-01 AND 51-40-02. REFERENCE BOEING DWG 65-54892 ID:0002 RSDR TSAA20211117015Scuff Plate · corroded1000573102 - BLENDED CORROSION ON R1 DOOR ATTACH ANGLE FOR LOWER SCUFF PLATE RBL 57 STA 294.5+4 TO STA 328. IAW B737-300 SRM 53-10-15 PG 113 DETAIL IX REV 125. FOUND TO BE BEYOND LIMITS NOM THICKNESS .090", .040" REMOVED, .050 REMAINING IAW B737-300 SRM 53-60-SDR TSAA20211117014Failsafe · broken1000573101- REPLACED FAIL SAFE ANGLE AT STA 420 STR 26L IAW REFERENCE BOEING DRAWING #65-46527 ID:0011 REV A & B737-300 SRM REV 125 CHAPTER 51-40-02 WITH MADE REPAIR PART.SDR TSAA20211117013Floorbeam · corroded1000573059 - CORROSION ON FLOORBEAM TOP CAP@ STA1006, RBL20 REPAIRED IAW AEI EO15495 REV IRSDR TSAA20211117012Floorbeam · corroded1000573058 - CORROSION ON FLOORBEAM TOP CAP@ STA 887 RBL 47 BLENDED I.AW B.737-300 SRM REV 125 CH
51-10-02 PARA 14 AND WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. ORIGINAL THICKNESS .153, MAX REMOVAL ALLOWED.015 (.138), REMAINING THICKNESS .079 I.AW B.737-300 SRSDR TSAA20211117011Anchor Fitting · corroded1000570383 - CORROSION UNDER ANCHOR NUT ON SUPPORT STRUCTURE FOR R/H AIR CON ACCESS PANEL @STA 566 RBL 42 WL 149, BEYOND LIMITS IAW B737-300 SRM REV 125 CH.57-10-13 FIG 101. SUPPORT BEAM LWR
CHORD REPLACED WITH MADE REPAIR PART FABRICATED AND INSTALLED IAW B7SDR TSAA20211117010Cargo Fitting · corroded1000570361 - CORROSION ON FWD CARGO PIT DUSTSILL WEB@ STA 420-STA 440 STR 26R REMOVED AND INSPECTED WITH A 10X MAGNIFYING GLASS I.AW B737-300 SRM REV. 125 51-10-02 PAR.14 NOMINAL THICKNESS:0.040", REMAINING THICKNESS: 0.033". MATERIAL REMOVAL OF 0.007" IS BEYOSDR TSAA20211117009Crease Beam · corroded1000570357 - CORROSION ON LOWER SURFACE ON CREASE BEAM WEB, STA 798 RBL 65 REMOVED AND INSPECTED USING A 10X MAGNIFYING GLASS IAW B737-300 SRM REV 125 51-10-02 PAR.14 NOMINAL THICKNESS
.032" REMAINING THICKNESS .024" MATERIAL REMOVED .008" IS BEYOND ALLOWABLESDR TSAA20211117008Channel · corroded1000570352 - CORROSION UNDER A/NON FLOOR SUPPORT CHANNEL, AFT CARGO PIT STA 773 LBL 3 REMOVED IAW B737-300 SRM REV 125 51-10-02 PARA 14A. NOMINAL THICKNESS .063", REMAINING THICKNESS .020".
MATERIAL REMOVAL OF .043" IS BEYOND THE ALLOWABLE LIMIT OF .0063" IAWSDR TSAA20211117007Keelbeam · corroded1000570259 - REPAIRED R/H KEEL BEAM LWR SURFACE@ STA 663.75-727, RBL 7, WL 148.5 IAW KF AEROSPACE DWG #R27904.1-053-023-001 REV:NC.SDR TSAA20211117006Beam · abnormal1000570256- REPAIRED L/H KEEL BEAM @STA 663.75-707, LBL 7, WL 148.5 IAW KF AEROSPACE DWG R27904.1-
053-022-001 REV:NC.SDR TSAA20211117005Intercostal · gouged1000567496- REMOVED GOUGES ON INTERCOSTAL ATTACH CLIPS X3@ STA 847 STR 20L, 21L, 19L IAW 8737-300 SRM REV 125 CH 53-00-04 FIG 101, MAXIMUM ALLOWABLE EDGE MATERIAL LOSS 0.100" EDGE MATERIAL REMOVED 0.089" IS WITHIN ALLOWABLE LIMITS IAW 8737-300 SRM REV 125 CH 5SDR TSAA20211117004Stringer Clip · broken1000565725 - REPLACED STRINGER CLIP@ STA 616 AT STR 9L IAW 8737-300 SRM REV 125 51-10-02 PARA 8 AND
INSTALLED IAW 8737-300 SRM REV 125 51-40-02 AND BOEING DOCUMENT #65-46539 REV:AV.SDR TSAA20211117003None · noneREPLACED STRINGER CLIP@ STA 727C STR 9L IAW B737-300 SRM REV 125 51-10-02 PARA 8 AND INSTALLED IAW 8737-300 SRM REV 125 51-40-02. AND BOEING DOCUMENTS #65C25228 REV:BK, AND
#65-73746 REV:CK.SDR TSAA20211117002None · noneBLENDED AND ASSESSED CORROSION ON BROWNLINE STA907-STA 1006 BL0 AND FOUND BEYOND ALLOWABLE LIMITS. NOMINAL THICK 0.280" REMOVED 0.034" REMAIN 0.246" IAW B737-300 SRM 53-00-52 FIG 101 DETAIL IX SECTION C-C REV 125. REPLACED BROWNLINE WITH MADE REPAIR PART IAW BSDR TSAA20211117001Structure · corrodedCORROSION ON FUSELAGE BELLY SKIN AT STA 727B, STR 26R FOUND TO BE BEYOND LIMITS IAW B737-300 REV 125 SMR 53-00-01, NOM THICKNESS OF 0.063", ALOWABLE REMOVEL 0.0063", REAMING THICKNESS 0.053", REPAIRED FUSELAGE BELLY SKIN AT STA 727B STR 26R IAW B737-300 REV 12SDR DU4R2021072920092Support Fitting · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LEFT WING AT MLG SYPPORT FITTING, HOLE #5 HAS A CRACK INDICATION IN CHORD LAYER. S/O 660006 N/R 38573SDR DU4R2021072200091Bulb · burned outDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND NUMBEROUS BULBS WERE OUT IN THE EMERGENCY EXIT LIGHTS ABOVE AND BELOW THE ENTRY DOORS. S/O 660006 N/R 38204.SDR DU4R2021071900090Skin · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L1 DOOR AT UPPER HINGE, HOLE AT BS 303.9, STR. 10L HAS TWO CRACK INDICATIONS. S/O 660006 N/R 39632SDR DU4R2021071900089Skin · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L1 DOOR FWD CORNER HAS CRACK INDICATION IN HOLE BS 304 - 6.5 INCHES, 2 INCHES DOWN FROM STR. 6L. S/O 660006 N/R 38447SDR DU4R2021070800087Skin · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND L/H WING, I/B UPPER SKIN, HOLE "B" 68, HAS A CRACK INDICATION. S/O 660006 N/R 38768SDR DU4R2021070800086Skin · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND L/H WING, I/B UPPER SKIN, HOLE "A" 100, HAS A CRACK INDICATION. S/O 660006 N/R 38767SDR DU4R2021070800085Skin · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H WING, I/B UPPER SKIN, HOLE "A" 75, AS A CRACK INDICATION. S/O 660006 N/R 38766SDR DU4R070800084Skin · corrodedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND LEFT WING UPPER SKIN ON THE LOWER SURFACE AT WBL 174.7, THE SKIN HAS CORROSION 1" FWD OF T/E OF SKIN. S/O 660006 N/R 38756SDR DU4R2021070200081Support · crackedDURING SCHEDULED INSPECTION, FOUND R/H MAIN LANDING W/W AFT BELLY CUTOUT RADIUS PANEL HAD A CRACKED PANEL SUPPORT. S/O 660006 N/R 38470SDR DU4R2021062400080Fitting · corrodedDURING SCHEDULED INSPECTION, FOUND LEFT MAIN LANDING GEAR FORWARD OUTBOARD LUG HAS SEVERE PITTING CORROSION. S/O 660006 N/R 38671SDR DU4R202106230078Panel · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H WING T/E AILERON, #3 AILERON HINGE FITTING, PANEL ATTACH BOLT HOLES HAVE CORROSION IN AND AROUND THEM. S/O 660006 N/R 38407SDR DU4R2021060900077Angle · dentedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND DENT IN FWD LWR ANGLE OF MAIN CARGO DOOR CUTOUT DOOR JAMB. S/O 660006 N/R 38238SDR DU4R2021060400076Bracket · puncturedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND WEB BRACKET HAS A PUNCTURE AT BS 344, STR. 16L. S/O 660006 N/R 38669SDR DU4R2021060400075Hinge Fitting · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H WING T/E AILERON, #2 AILERON HINGE FITTING, PANEL ATTACH BOLT HOLES, HAVE CORROSION IN AND AROUND THEM. S/O 660006 N/R 38406SDR DU4R2021051700074Floor Panel · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CARGO COMPARTMENT FLOOR PANEL 1534X HAS MULTIPLE AREAS OF SURFACE ETCH CORROSION. S/O 660006 N/R 38253SDR DU4R2021051400072Structure · damagedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND A DENT AND CRACK IN THE L/H TRAILING EDGE OF THE MID FLAP THAT WAS STOP DRILLED AND SEALED. S/O 660006 N/R 38151SDR DU4R2021050700071Shear Web · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND SHEAR WEB FRAME 592.4 OF FWD CARGO DOOR AFT FRAME IS CRACKED. S/O 660006 N/R 38630SDR DU4R2021050700070Transition Panel · corrodedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CARGO COMPARTMENT, BS 727D +10 - 790 LBL 24 TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION AND 2 EACH LOOSE FRAME ATTACH RIVETS. S/O 660006 N/R 38261SDR DU4R2021050400069Attach Angle · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MULTIPLE AREAS OF CORROSION ON FLOOR PANEL CROSS ATTACH ANGLE IN AFT CARGO COMPARTMENT AT BS947.5, LBL-24 - RBL-24. S/O 660006 N/R 38282SDR DU4R2021050300068Attach Fitting · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H MLG SUPPORT BEAM STABILIZER ATTACH FITTING HAS FRETTING ON BOTH LUG FACES. S/O 660006 N/R 39463SDR DU4R2021050300067Transition Panel · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND TRANSITION PANEL IN AFT CARGO COMPARTMENT, AT BS 787 TO BS 947.5, LBL 24, HAS MULTIPLE AREAS OF CORROSION. S/O 660006 N/R 38264
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