Boeing 737-924ER
Service difficulty reports · 3,678
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 = '737924ER' 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 = '737924ER' 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 CALA2026083119085Skin · crackedRIGHT HORIZ STAB LOWER SKIN IS CRACKED ON THE INBD SIDE OF THE RIB AT STAB STA 147.9 APPROX 15" FWD OF THE AFT SPAR. COMPLETED REPAIR AT RT HORZ STAB HSS 147.9 IAW SRM 55-10-01-2R-11, REPAIR II. A CATEGORY B REPAIR.SDR CALA2026083119082Skin · fomRIGHT HORIZONTAL STAB LOWER SKIN AT STA 92.70 REQUIRES CUT OUT TO FACILITATE RIB REPAIR ON CARD 9282739. COMPLETED ESFR FOR ACCESS CUT OUT FACILITATION REPAIR ON RT HORIZONTAL STAB SKIN AT HSS 92.70 NO ISSUES NOTED. COMPLETED REPAIR AT HSS 92.70, RT HORZ STABSDR CALA2026083119080Skin · fomRIGHT HORIZONTAL STAB LOWER SKIN AT HSS 111.10 REQUIRES CUT OUT TO FACILITATE RIB REPAIR ON CARD 9282740. COMPLETED ESFR FOR HORIZONTAL STAB SKIN REPAIR. NO ISSUES NOTED. COMPLETED REPAIR AT HSS 111.10 RT HORZ STAB IAW SRM 55-10-01-2R-11, REPAIR II. IT'S ASDR CALA2026060516855Lens · missingSEAT 20ABC WHITE EMERGENCY PATH LIGHT INOP AND MISSING LENS. CORRECTION, LIGHT LENS SHOULD BE RED, REF DWG 3350DD15107_A. SEAT 20ABC HAS TWO RED EMER PATH LIGHTS, THE AFT LIGHT IS INOP AND HAS A MISSING LENS. REMOVED AND REPLACED SEAT 20ABC AFT RED EMERGENCY LSDR CALA2026060816918Stringer · damagedSTRINGER 20L BETWEEN STA 847 AND 867 DAMAGEDREMOVED DAMAGE SECTION OF STRINGER AS PER SRM STRINGER 20L DAMAGED BETWEEN STA 847 AND 867 VERIFIED DAMAGED STRINGER IS REMOVED. MATERIAL ID FOR NEW STRINGER FABRICATED SECTION 146A3204-82. SEE WORK FOR FOR ALL WORKSDR CALA2026060816920Skin · damagedFUSELAGE SKIN DAMAGE AT STR20L- STA847-867. REMOVED DAMAGE TO EVALUTE 11.75 L X 5.125 W REMOVED DAMAGE AREA OF THE FUSELAGE SKIN. RECTANGLE WITH THE SIDES PARALLEL AND PERPENDICULAR TO THE STRINGER SRM 53-00-01-2R-36 REPAIR INSTRUCTIONS 4. (C) ADD EMP:U347143SDR CALA2026060516850Smoke Detector · faultedFWD LAV SMOKE DETECTOR WENT OFF IN FLIGHT NO SMOKE OR SMELL OF SMOKE PRESENT. PERFORMED FWD LAV A SMOKE DETECTOR SELF TEST AND SMOKE TEST REF AMM 26-14-00. BOTH OPS CHECK GOOD AT THIS TIME.SDR CALA2026060516835Seal · crackedR/H HORIZONTAL STAB FWD UPPER SLIDING SEAL IS CRACKED AT THE CONTACT POINT OF THE SLIDE TRACK. TRANSCRIBED FROM AAR GSO NRC 9282733. REMOVED AND REPLACED R/H HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW B737-900 AMM 53-31-31 AND SRM 51-40-02. IAW AMM 53-31-31. SDR CALA2026060416820Seal · crackedLEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL IS CRACKED AT THE CONTACT POINT OF THE SLIDE TRACK. . REMOVED AND REPLACED L/H HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-53.SDR CALA2026060416816Battery Pack · no testOPS CHECKED EMERGENCY LIGHTS, DOOR 2R EMERGENCY EXIT SIGNS AND SLIDE LIGHT ARE INOP. ACCOMPLISHED BATTERY PACK REPLACEMENT PER MM33-51-06-960-805. OPS CK OK.SDR CALA2026060316783Scuff Plate · crackedAFT CARGO PIT CORNER SCUFF PLATE 140AF1 IS CRACKED. LOCATED, DRILLED AND COUNTERSUNK AFT CARGO PIT CORNER SCUFF PLATE 140AF1 IAW SRM 51-40-05 AND BAC DWG 146A8341 REV-. LOCATED,DRILLED & COUNTERSINK AFT CARGO PIT CORNER SCUFF PLATE 140AF1 IAW SRM 51-40-05 & SDR CALA2026060316774Battery · faultedLFT FWD FA FLASHLIGHT INOPERATIVE T/S AND REPLACED L-1 DOOR FLIGHT ATTENDENT STATION OTBD EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00-900-806. FLASHLIGHT TEST GOOD, OK FOR SERVICE.SDR CALA2026060316768Transition Panel · corrodedFWD PIT TRANSITION PANEL UPPER SURFACE HAS CORROSION FROM STA 500D - 500L, LT SIDE. REMOVED AND REPLACED FWD PIT TRANSITION PANEL FROM 500D TO 500L LH SIDE IAW SRM 51-40-02 AND DWG 143A7500. REV B.SDR CALA2026060316766Baffle · cracked(SUPPORT TASK): FWD CARGO PIT L/H SIDE AT STA 500K (AFT) HAS A CRACKED BAFFLE CLIP. REMOVED AND REPLACED BAFFLE CLIP ON FWD CARGO PIT L/H SIDE AT STA 500KI (AFT) IAW B737-900ER SRM 51-40-02 AND BAC DWG # 143A7505 REV -.SDR CALA2026060216750Skin · crackedSUPPORT TASK: RH O/B AFT FLAP LOWER SKIN AT I/B TRACK HAS CRACK AT DRAIN HOLE.TRANSCRIBED FROM AAR GSO NRC 9282672. RECEIVED NEW RIGHT WING OTBD AFT FLAP ASSY PN#113A3700-24UAL FLAP ASSY REMOVED AND REPLACED ON AAR GSO NRC 9282690. AAR GSO MECH V896730 ALL MASDR CALA2026060216748Battery Pack · inoperativeEPS BATTERY FAILD OP CHECK SDR REPORTING ONLY THE SDR HAS BEEN NOTED THE THE ELB LOG PAGE.REPLACED EPS BATTERY PACK AT STA 952 WL 290 LBL 14 IAW AMM 33-51-06-960-805 OP CHECK GOOD.SDR DALA2026060203354Battery Pack · inoperativeLT AFT OW EXIT EMERGENCY LIGHT NOT ILLUMINATED. R & R BATTERY PACK AT LOCATION M1694 IAW AMM 33-51. OPS CHECK GOOD. (LOG 8630897 - AIRCRAFT WAS GROUNDED).SDR CALA2026060216756Light · inoperative34C EMERGENCY INOP SEAT MOUNTED EXIT PATH LIGHT INOP AT SEAT 34C ONLY REQUEST MEL. TOMC APPROVED COMPLIED WITH MEL. REMOVED AND REPLACED 34C EMERGENCY PATH LIGHT IN REF TO AMM 33-51-11. OPS CHECKS GOOD AT THIS TIME. PLACARD REMOVED.SDR CALA2026060216755Wire Harness · damagedEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - FLOOR PROXIMITY LIGHT AT SEAT 26C INOP REPLACED WITH SERVICEABLE WHITE PROXIMITY FLOOR LIGHT, NO HELP. PUT ORIGINAL LIGHT BACK ON. SUSPECTED SEAT HARNESS NIS AT LAS REQUESTING DEFERRAL ASDR CALA2026060116725Skin · crackedLEFT WING INBD L/E SKIN HOLES NR 10 AND 11 HAVE CRACK INDICATIONS. FABRICATED DOUBLER AND FILLER IAW UAL ECRA 5720-03641 AND SRM 57-41-01-2R-8 REPAIR 8. INSTALLED DOUBLER AND FILLER PER B737-900ER SRM 57-41-01-2R-8 REPAIR 8 AND ECRA 5720-03641.SDR CALA2026060116723Skin · crackedRIGHT WING INBD L/E SKIN HOLE NR 12 HAS A CRACK INDICATION. REPAIRED RT WING L/E SKIN AT HOLE NR 12 WITH FILLER AND DOUBLER AND APPLIED PROTECTIVE FINISHES IAW SRM 57-41-01 AND 51-20-01.SDR CALA2026060416806Rib · crackedSUPPORT TASK RH HORIZONTAL STAB INBD SIDE OF RIB AT STAB STA 111.10 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 3 VERTICAL STIFFENER. CUT AND REMOVED THE DAMAGE FROM THE RIB AND WEB AS SHOWN IN FIGURE 2026 REPAIR 4 IAW SRM 55-10-09-2R-4. FABRICATED SDR CALA2026060416804Rib · crackedRH HORIZONTAL STAB INBD SIDE OF RIB AT STAB STA. 92.70 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NO 2 VERTICAL STIFFENER. CUT AND REMOVED THE DAMAGE FROM THE RIB AND WEB AS SHOWN IN FIGURE 202 REPAIR 4 IAW SRM 55-10-09-2R-4. FABRICATED REPAIR PARTS -1SDR CALA2026060116715Fscu · faultedFLAPS FAILED TO RETRACT PAST 5 ON DEPARTURE. CREW ERROR WENT PASSED DETENT INTENDED TO FAST AND LOCKED OUT FSCU. RESET CIRCUIT BREAKER OF FSCU, ALL FLAPOPERTIONS NORMAL. REF FIM 32-09 814. PER THE CAPTAIN HE STATED TOOK OFF AT FLAPS 5 FLAP LEVER WAS NOT IN TSDR CALA2026060116703Floor Panel · corrodedFWD CARGO PIT FLOOR PANEL 120DF HAS MULTIPLE GOUGES AND CORROSION. THE DISTANCE BETWEEN DAMAGES ON FLOOR PANEL 120DF IS LESS THEN 5", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. REPLACED FWD CARGO PIT FLOORPANEL 120DF IAW GMM 07-35-05. R&R FLOORBOARDSDR CALA2026060116664Oven · dirtyFA REPORTS AFT GALLEY OVEN 425 HAS BAD SMELL CLEANED GALLEY OVEN 425 REF. AMM 25-34-00. OPS CHECK SAT. SMELLS NORMAL AFTER CLEANING.SDR CALA2026060116714Elec Connector · faultedELEC HYD PUMP A OVERHEAT INFLIGHT ON DEPARTURE REMOVED AND REPLACED HYDRAULIC SYSTEMS A ELECTRIC MOTOR-DRIVEN PUMP (EMDP) ACOUSTIC FILTER IN REF TO AMM 29-11-27. REMOVED AND REPLACED ELECTRIC MOTOR-DRIVEN PUMP (EMDP) SYS A IN REF TO AMM 29-11-21. REMOVED AND SDR CALA2026060116701Floor Panel · corrodedAFT CARGO PIT FLOOR PANEL 140CF HAS MULTIPLE GOUGES ANDEE CORROSION. DISTANCE BETWEEN DAMAGES ON FLOOR PANEL 140CF IS LESS THAN 5" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW AFT CARGO PIT FLOOR PANEL 140CF IAW GMM 07-35-05 STEP 3C (8).SDR CALA2026060116699Floor Panel · corrodedAFT CARGO PIT FLOOR PANEL 140AF HAS MULTIPLE GOUGES AND CORROSION. DAMAGE OUT OF LIMITS. FABRICATED ALODINED AND PRIMED AFT CARGO FLOOR PNL #140AF IAW SRM 53-00-53, SRM 53-60-53, AND SRM 51-20-01.SDR CALA2026060116696Floor Panel · corrodedFWD CARGO PIT FLOOR PANEL 120CF HAS MULTIPLE GOUGES AND CORROSION ON UPPER SURFACE. THE DISTANCE BETWEEN DAMAGE ON FLOOR PANEL IS LESS THAN 5" FOUND TO BE OUT OF LIMITS IAWSRM 53-00- 53-1A-1 AND FABRICATED NEW FLOOR PANEL 120ZF IAW GMM 07-35-05. ALODINED AND PSDR CALA2026060116693Floor Panel · corrodedAFT CARGO PIT FLOOR PANEL 140EF HAS MULTIPLE GOUGES AND CORROSION. AFT CARGO FLOOR PANEL 140EF FOUND TO BE OUT OF LIMITS. MAT ID 2024-T3 TYPE .071 SH ALUMINUM PO: 1143752.2 FABRICATED FLOOR PANEL IAW SRM 51-40-02 AND UNITED GMM 07-35-05.SDR CALA2026052916656Transition Panel · corrodedFWD CARGO BAY TRANSITION PANEL UPPER SURFACE CORRODED BS 500A - 500L, RT SIDE. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL THICKNE SS: 0.040" MATERIAL LOSS: 0.006" REMAINING THICKNESS 0.0.4", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 AND BAC1496-444. SDR CALA2026052916654Baffle · crackedFWD CARGO BAY, BS 500J LT BAFFLE ANGLE (AFT) CRACKED. R & R BAFFLE ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV -.SDR CALA2026052916650Baffle · corrodedFWD CARGO LOWER BAFFLE CORRODED ON LOWER SURFACE OF UPPER FLANGE. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL THICKNESS: 0.020" MATERIAL LOSS 0.004" REMAINING THICKNESS 0.016", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FWD CARGO BSDR CALA2026060116691Floor Panel · corrodedFWD CARGO PIT FLOOR PANEL 120EF HAS MULTIPLE GOUGES AND CORROSI9ON. FOUND DAMAGE OUT OF LIMITS-DISTANCE LESS THAN 5"- FABRICATED, ALODINED, PRIMED FLOORPANEL 120EF NEW PANEL AT FWD CARGO PIT IAW B737 SRM 53-00-53, SRM 51-20-01, SRM 51-40-05 AND UAL GMM 07-35SDR CALA2026060116687Support Bracket · corrodedAPU DOOR INSULATION SUPPORT BRACKET (5EA) IS CORRODED. COMPLETED NO ALLOWABLE DAMAGE FOUND FOR SUPPORT BRACKETS 5EA IAW SRM 51-10-02-0G-0 STEP 9C REMOVED AND REPLACED APU DOOR INSULATION SUPPORT BRACKETS 5EA IAW B737-900ER SRM 51-40-02 BAC DWG 148A6350 REV A SDR CALA2026052816599Wire Harness · brokenCABIN EMERGENCY AISLE ROW 5AB LIGHT INOP FIRST CHANGED LIGHT BULB, NO HELP. THEN CHANGED THE LIGHT ASSEMBLY AND IT'S STILL INOP. DURING INITIAL EVALUATION WAS FOUND ROW 5AB EPL HARNESS BROKEN, REMOVED AND REPLACED ROW 5AB EPL HARNESS ASSY IAW CMM 25-22-51-3671SDR CALA2026060416802Rib · crackedRIGHT HORIZONTAL STAB RIB AT STA 129.5 LOWER O/B FLANGE HAS A CRACKED FASTENER HOLE AT APPROX 28.5" AFT OF THE FWD SPAR. REPAIRED DAMAGED RIB IAW B737 SRM 55-10-09-2R-5. REPAIRED DAMAGED RIB IAW B737 SRM 55-10-09-2R-5 AT RT HORIZONTAL STAB AT STAB STA 129.5SDR CALA2026052616536Fuse · faultedRED EPL LIGHT ON ROW 20 LENS SMASHED REMOVED AND REPLACED RED EPL IN REF CMM 3350DD15295. UPON OPS CHECK EMERGENCY PATHWAY LIGHTS DID NOT OPERATE FOLLOWING FIM 33-50 TASK 801 CHECKED L SIDE EMERGENCY POWER SUPPLY AND REMOVED AND REPLACED THE BATTERY IN REF IPCSDR CALA2026052516516Panel · corrodedNLG WHEEL WELL PANEL 114BW HAS SURFACE CORROSION ADJACENT TO ATTACHMENT FASTENER. EVALUATED PANEL ASSY TO BE BEYOND REPAIRABLE LIMITS IAW B737 SRM 53-10-14. RECEIVED REPLACEMENT PANEL AIPC 32-22-11-02 ITEM 35 FOR EFFECTIVITY. EVALUATED PANEL ASSY TO BE BEYSDR CALA2026052516514Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ON AFT RIGHT SERVICE DOOR NOT ILLUMINATING. TROUBLESHOOT WITH AWD 33-51-14-5 SUSPECTED BAD BATTERY , SLAVED IN BATTERY FROM LEFT SIDE, LIGHTS WORKED NORMALLY , PUT LEFT BATTERY BACK AND REMOVED THE INOP RIGHT SIDE BATTERY FROM AC, CORRISSDR CALA2026052716565Structure · damagedFWD GALLEY WALL BY OVEN 205 DISCOLORED. VERIFIED OVEN 205 NOT LEAKING TO THE WALL. REMOVED OVEN FOR RAMS TEAM REF AMM 25-34-00 REMOVED DAMAGED DECO MATERIAL, WALL NOT DAMAGED, INSTALLED NEW DECO MATERIAL REF CMM 25-32-43. REINSTALLED FWD GALLEY OVEN 205 REF SDR CALA2026052516510Tube · crackedLH ENGINE FIRE SUPPRESSION TUBE IS SHEARED. LOCATED APPROX 9" INBD OF ENG AFT PYLON FAIRING REMOVED AND REPLACED LEFT ENGINE AFT FIRE SUPPRESSION TUBE THAT RUNS THRU PANEL 551GB IAW BOEING DRAWING 272A3101-13 REV B AND AMM 26-21-00-720-801.SDR CALA2026052516506Wire Harness · frayedDURING SERVICE CHECK FOUND 2ABC AISLE LIGHTA INOP BOTH SEAT 2ABC EMERGENCY AISLE LIGHT ARE INOP. REPLACED AFT AISLE LIGHT ON SEAT 2ABC AND RELAMPED BOTH LIGHTS NO HELP REF AMM 33-51-11 NO TIME FOR FURTHER TROUBLESHOOTING REQUEST DEFERRAL MEL 3319E BOTH LIGHSDR CALA2026052816591Floor Panel · corrodedAFT CARGO PIT FLOOR PANEL 140BF HAS MULTIPLE GOUGES AND CORROSION. FABRICATED NEW FLOOR PANEL 140BF, GOUGE OUT OF LIMITS. APPLIED ALODINE AND PRIME IAW SRM 53-00-53-1A-1, 53-60-53-0I-1, 51-20-01 AND GMM 07-35-05.SDR CALA2026052616527Power Supply · inoperativeEMERGENCY LIGHTS - OPS CHECK EMERGENCY LIGHTS, OVERHEAD MOUNTED AISLE LIGHTS, RT AFT ESCAPE EXTERIOR LIGHT, & RIGHT OVERWING ESCAPE GROUND ILLUMINATION LIGHT (L00007, L00548, L01507, L01513, L01517) INOP. SLAVED IN NEW EMERGENCY BATTERY PACK, NO HELP. REPLACESDR CALA2026052516504Clevis · corrodedLEFT HORIZONTAL STAB LOWER K LUG FOUND WITH CORROSION DURING REMOVAL DUE TO FREE PLAY CHECK FAILURE. REMOVED CORROSION AND REWORKED AREA ON LH HRZ STAB REAR SPAR LOWER CLEVIS FITTING IAW EC/RA5510-03374.SDR CALA2026052516502Stub Beam · gougedR2 DOOR HANDLE BOX CUTOUT, LOWER STUB BEAM IS GOUGED. REMOVED DAMAGED LOWER STUB BEAM IAW SRM 51-40-02 AND INSTALLED NEW STUB BEAM IAW SRM 51-40-02 AND APPLIED TOP COAT IAW AMM 51-21-73 AND DWG 147A6502 REV A.SDR CALA2026052516500Skin · gougedR2 DOOR LOWER HINGE ARM ACCESS PANEL AREA, LOWER EDGE IS GOUGED. REMOVED DAMAGED LOWER INNER SKIN IAW SRM 51-40-02 AND INSTALLED NEW LOWER INNER SKIN IAW B737-900ER SRM 51-40-02 AND APPLIED TOP COAT IAW AMM 51-21-73.SDR CALA2026052516498Hinge Fitting · corrodedWEAR WAS FOUND ON RH HORIZONAL STAB HINGE FITTING. WEAR WAS DISCOVERED UPON REMOVAL OF RH STAB DUE TO FREE PLAY CHECK FAILURE. PERFORMED REPAIR OF HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER RH HINGE FITTING (P/N 181A1110-1) CLEVIS IAW ECRA5510-03375.
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