JASC 5100
Service difficulty reports · 4,224
Reports filed under 5100 · Standard Practices/Structures, newest first.
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 jasc_code = '5100' 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 jasc_code = '5100' 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 SWIA2026040877440Frame · fomREMOVE AND SPLICE FRAME FS 485, STR20R FROM STR26R TO FOM. PERFORMED SPLICE REPAIR OF FRAME AT FS485, STGR26R - STGR20R REF REO 670-53-31-1193 REV -, SRM 53-00-06-201-001-A03, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-33200 REV G.SDR SWIA2026040877435Frame · fomREMOVE AND SPLICE FRAME FS 469, STR20L FROM STR23L TO FOM C-CHECK RO 09302026REMOVED AND SPLICED FRAME FS469, FROM STR20L TO STR23L BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2857 REV -, SRM 53-00-06-201-001-A03 , SRM 51-42-21-001-001-A01, 51-42-06-001-001SDR IPXA2026050796878Bracket · crackedPANEL 334ET, BRACKET HAS A CRACK. INSTALLED NEW ANGLE (BRACKET) I.A.W A300-600 SRM 51-40-21.SDR DALA2026041402347Not Reported · not reportedREFERENCE ER/A626909-14AD. COMPLIED WITH ER/A626909-14AD (1533159) (AIRCRAFT GROUNDED)SDR HNAA20260800277Not Reported · not reportedW/SPS ADVANCED IN FLIGHT.SDR DALA2026040802240None · nonePERFORM INSPECTIONS PER ERA 628936-14. C/W ER/A 14-628936. (1525444) (AIRCRAFT GROUNDED)SDR IPXA2026040172052None · noneALL FOUR OVERWING EMERGENCY SLIDE LIGHTS ARE INOPERATIVE. LEFT AND RIGHT WINGS IAW ENGINEERING, LIGHTS WERE DEACTIVATED DURING P TO F CONVERSION IAW SB 747-00-2117. NO FURTHER ACTION NEEDEDSDR DALA2026040202140None · noneER/A 624580-14 / AMOC RESTRICTION FOR AD 2025-03-06. ER/A 624580-14 / AMOC RESTRICTION FOR AD 2025-03-06. ER/A 624580-14, REV C / REPAIR APPROVAL IS LIMITED TO 48,000 TOTAL FLIGHT CYCLES. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CSDR DALA2026040202139None · noneER/A 624580-14 / SECTION II INSPECTIONS. ER/A 624580-14, REV C / AT, OR PRIOR TO 14,000 FC FROM SECTION I REPAIR (50,705 TOTAL FLIGHT CYCLES), AND REPETITIVELY EVERY 4,000 FC THEREAFTER, ACCOMPLISH SECTION II INSPECTIONS. (LP: 1520491) AIRCRAFT WAS GROUNDED.SDR DALA2026040402153Not Reported · not reportedPERFORM ER/A 632197-14 FOR GAIN ACCESS TO REPLACEMENT CONTINUITY FITTINGS LT & RT. COMPLIED WITH ER/A 632197-14 REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 632197-14 PRI REV 0 IT IS BEEN VALIDATED, PERFORMED REPAIR INSTRUCTIONS FOR GAIN ACCESS TO REPLACEMENT SDR DALA2026033102102Frame · not reportedLEFT HAND STA 727 FRAME INNER CHORD , 737 REPAIR; RII; SECTION 2 IN REF TO THE AMDS 5311-01251-02A. ACCOMPLISHED IN REF TO THE AMDS 5311-01251-02A STEP 13. (LOG 1517104)SDR DALA2026033102101Frame · not reportedRIGHT BS 727 FRAME INNER CHORD,737 REPAIR; RII; SECTION 02 IN REF TO THE AMDS 5311-01251-02B. ACCOMPLISHED IN REF TO THE AMDS 5311-01251-02B STEP 13. (LOG 1517089)SDR N6WA202503270002None · noneREJECTED TAKE OFF. PERFORMED REJECTED TAKE OFF INSPECTION IAW CRJ AMM 05-51-27. NO DEFECTS NOTED.SDR MAS2026F00004Battery · firePASSENGER AT SEAT 3D PORTABLE CHARGER CAUGHT FIRE/ PERFORMED AMM CHECK FOR SMOKE/ ABNORMAL SMELL NFDN. A/C OUTLET ON 3D HAS SCORCH MARKS NEEDS AN INSPECTION/ PLACED ON MEL. HALON FIRE EXTINGUISHER FWD WAS USED. R&R FWD FIRE EXTINGUISHER. CONTAINMENT BAG ANSDR MASA2026032500011Battery · firePASS BATT CAUGHT FIRE AT 3D/EMER DECLASDR UIEA2026031100082Not Reported · not reportedWHILE ACCOMPLISH EO #4453C592, FOUND STEP 1 TBD BY EO REV 1 AND REQUIRE TO CONTACT MANUFACTURER TO APPROVE THE EXISTING REPAIR AND PROVIDE THE CAT B FAA 8100-9. REPAIR CARRIED OUT IAW EN #3137-26 REV 1. NO FURTHER DEFECTS NOTED.SDR DALA2026032602009Stop Fitting · not reportedPASSENGER CABIN AT FR68 AFT FACE AREA, BETWEEN STGR21R AND STGR23R, LEVEL DOOR STOP 1 FOUND REPAIR FITTING INSTALLED. WORK CARD 5311-01244-02B, SB A320-53-1491. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTION THAT MAY BE REQUIRED TO COMPSDR DALA2026032501992None · noneERA 633129-14 SECTION I ISSUED FOR REPAIR TO BS 1076, L14R SKIN FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 633129-14 (1510528)SDR DALA2026032602008Fitting · not reportedDTE ERA 632268-14AD REV. ORIGINAL. REPLACEMENT OF CONTINUITY FITTING IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 61,196 TFC. REVISE AND UPDATE ERA 632268-14AD WITH DTE RESULTS PRIOR TO 61,196 TFC. REFERENCE AIRBUS DOSSIER 81739836. ASSOCIATED AA 5311-01SDR DALA2026032602007Fitting · not reportedTE ERA 632195-14AD REV ORIGINAL. REPAIR AT MIRROR FITTINGS, AREA 3 IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 91,696 TFC. REVISE AND UPDATE ERA 632195-14AD WITH DTE RESULTS, PRIOR TO 91,696 TFC. ASSOCIATED AA 5311-01226 ADDED FOR AC 3165 ASSOCIATED ER/SDR DALA2026032602006Not Reported · not reportedINSPECTION ERA 632195-14AD REV. ORIGINAL. REPAIR OF WINDSHIELD FRAMING AREA 2 REQUIRES FOLLOW-ON INSPECTIONS PRIOR TO 58,696 TFC AND EVERY 4,700 FC, THEREAFTER. ACCOMPLISH FOLLOW-ON INSPECTIONS PER ERA 632195-14AD SECTION II PRIOR TO 58,696 TFC AND EVERY 4,70SDR IPXA2026032075072Elevator · not reportedADD SDR FOR UPS EO-85445-JIC2 (REPLACE) ADD SDR FOR EO-85445-JIC2 , THE SDR NO.T3F18E008H8PL. JOB COMPLETED.SDR IPXA2026032075165Elevator · not reportedADD SDR FOR UPS EO-85445-JIC1 (REPLACE) 1.ADD SDR FOR EO-85445-JIC1 , THE SDR NO.T3F18E008H8S1 2.JOB COMPLETED.SDR FDEA202603200361None · noneREF WRI 56-11 /8255 , C/OUT RTO / HIGH ENERGY STOP INSP. RTO / HIGH ENERGY INSPECTION C/OUT IAW B777 AMM 05-51-14-2-0 , FOUND SATIS. A/C OK TO SVC ALL BRAKE TEMPS WITHIN DISPATCHABLE LIMITS.A/C OK FOR SVCSDR SCNA20260323129Structure · unsecureL2 LAV DOOR ASHTRAY IS LOOSE AND HAS SHARP EDGE. SECURED ASHTRAY AND REMOVED SHARP EDGES B737 CM 25-46-11SDR CALA2026082718966Skin · fomLEFT HORIZONTAL STAB LOWER SKIN AT BS 92.70 BETWEEN NR 2 & 3 VERTICAL STIFFENER REQUIRES CUTOUT TO FOM. COMPLIED WITH CUTOUT LOWER SKIN AT STA 92.70 BETWEEN NR 2 & 3 VERTICAL STIFFENERS IAW SRM 55-10-01-2R-11. ACCOMPLISHED SURFACE HFEC IN SP OF CUTOUT & AREASDR SWAA2026031679966Unknown · noiseTHUMP NOISE HEARD ON TAKEOFF FROM FLL. NO ABNORMAL VIBRATIONS. NORMAL SMOOTH LANDING. NORMAL TAXI TO GATE. NO VISUAL DEFECTS NOTED ON WALK AROUND. PERFORMED WALK AROUND AND NOSE LANDING GEAR INSPECTION PER AMM 32-21-00 NO DEFECTS FOUNDSDR SWIA2026031477417Frame · fomREMOVE AND SPLICE THE FRAME AT BS 485, STR 16L - 20L TO FOM. REPAIRED FRAME AT BS 485 ,STR 16L - 20L BY COMPLYING WITH ALL STEPS OF REO 670-53-00-824 REV -, SRM 53-00-06-201-001-A03, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-33100, RESDR SWIA2026031477345Frame · fomREMOVE AND SPLICE FRAME FS 465, STR16L FROM STR20L TO FOM C-CHECK RO 9302026DISCREPENACY ERROR FRAME FOUND TO BE FS 469 REMOVED AND SPLICED FS469 FROM STR16L TO STR20L BY COMPLYING WITH ALL STEPS OFREO 670-53-00-824 REV -- DATE2026-04-07 AND REF DWG SH670-31SDR SWIA2026031377465Frame · fomREMOVE AND SPLICE FRAME AT BS 501, STR 16 - 20R TO FOM. INSTALLED NEW FRAME SECTOR IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, SRM 53-00-06-201-001-A03, AND DWG SH670-33101, REV J.SDR SWIA2026031377448Frame · fomREMOVE AND SPLICE FRAME FS 485, STR16R FROM STR20R TO FOM. PERFORMED SPLICE REPAIR ON FRAME AT FS485, STGR 16R - 20R REF REO 670-53-31-1188 REV -A, SRM 53-00-06-201-001-A03, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-33101 REV J .SDR CALA2026031614596None · noneBIRD STRIKE CAPT WINDSCREEN, INSPECTED CRAFT FOR DAMAGE, NO DAMAGE TO REPORT, CLEANED BIRD DEBRIS AND BLOOD FROM WINDSHEILD, RADOME AND CROWN CLOSEST TO CAPT WINDSHEILD REF AMM 05-51-18-210-801.SDR DALA2026031301763Bracket · wrong partDRAWING G5397629600200 SECTION C-C WRONG BRACKET PER DRAWING. CORRECTED PER ERA 632216-14 REV. ORIG. (1491175)SDR DALA2026031701822None · noneENSURE INCORPORATION OF FAA APPROVAL OF CDCCL REQUIREMENTS IAW ERA 631584-14AD. FAA RESTRICTION LIFTED AND APPROVAL GIVEN REF ER/A 631584-14AD. (8169946)SDR HNAA2026031100210None · noneHEAVY FUEL ODOR IN AIRCRAFT WITH APU RUNNING. INSPECTED FOR DEFECTS, NONE NOTED. SUSPECT FUEL ODOR WAS CAUSED DURING REFUELING OPERATIONS. FUEL ODOR SUBSEQUENTLY DISSIPATED W/PACS RUNNING. OK FOR SERVICESDR CALA2026090119146Repair · inspectedINSPECT THE REPAIRED AREA OF FUSELAGE SKIN AT L1 DOOR CUTOUT AFT LOWER CORNER PER THE LATEST REVISION OF EC/RA 5315-01195 PART 2SDR SWIA2026030877341Frame · fomREMOVE AND REPLACE FRAME FS333 STR20R TO STR20L TO FOM C-CHECK RO 9302026REMOVED AND REPLACED FRAME WITH NEW PART AT FS333 STR20R TO STR21L REF DWG SH670-32420 REV E AND CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 COMPLIED WITH ALL STSDR DALA2026031001645Not Reported · not reportedSHIP 9523 ERA 632996-14 ISSUED FOR REPAIR TO STA 207-218,L L17-18RH. CORRECTIVE ACTION: REPAIRED PER ERA 632996-14. (1485115)SDR AALA202603100296Insulation · contaminatedAIRCRAFT WAS GROUNDED: VOMIT SMELL COMING FROM AIRCRAFT AIR CONDITIONING SYSTEM. WHILE ACCOMPLISHING TROUBLE SHOOTING OF SOF EVENT FOUND RECIRCULATION FAN FILTERS TO BE DIRTY AND FOUND RECIRCULATION FAN INSULATION BLANKETS COVERED IN UNKNOWN LIQUID. REMOVED ANSDR YENA2026030900283Ped · odorFLT# 1437 BDL- MCO. " BURNING SMELL NOTED BETWEEN ROWS 11-15 AIRCRAFT RIGHT. TURNING OFF THE PED POWER ELIMINATED THE SMELL.; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEPS 1 AND 2. IDENTIFIED ODOR TYPE 9-ELECTRICAL. REF LOGPAGE 4458537-2 FOR CORRECTIVE ACTISDR DALA2026031001632Stringer · noneREF AMDS 5311-01244-02A FR68 LH AT STGR22 PREVIOUS REPAIR INSTALLED (ERA 542044-14). COMPLIED WITH ER/A 542044-14AD REV. A SECTION VI AND AMDS 5311-01244-02A. (LP: 1481872)SDR DALA2026031001644Not Reported · not reportedSHIP 9577 ER/A 631995-14AD REV ORIGINAL REQUIRES STAGE 2 & 3 DTA APPROVAL. REPAIR ACCOMPLISHMENT PER ER/A 631995-14AD (1480809)SDR DALA2026030801592None · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 13 RH SIDE AT Z = 1330 IN PASSENGER CABIN (REFERENCE AA CARD 5100-01821-01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 13 RH SIDE AT Z = 1330 IN PASSENGER CABIN AND FOUND MEETS THE GENERAL REQUISDR DALA2026030501535None · noneNEED TO DRILL SUPPORT BRACKETS TO REROUTE COAX CABLE, COAX IN WRONG SPOT. CORRECTED PER ERA 632216-14 REV. ORIG. (1480270)SDR SWIA2026030476630Frame · fomFRAME AT BS 333. REQUIRES CUT OUT DUE TO MULTIPLE STRINGER REPLACEMENTS. PERFOMED REPAIR AT FRAME BS 333 IAW AMM 20-70-00, SRM 51-42-06, 51-42-13, 51-42-21, IAW REO 670-53-21-799 REV -A.SDR DALA2026031001648Not Reported · not reportedER/A 627199-14AD REV F REQUIRES STAGE 2 DTA APPROVAL. REPAIRED PER ER/A 00-627199. (1478991)SDR DALA2026031001627Window Frame · noneINSPECTION ERA 631653-14AD REV ORIGINAL. WINDSHIELD FRAMING ( AREA 2) REQUIRES FOLLOW UP INSPECTIONS PRIOR TO 58,114 TFC AND EVERY 4,700 FC THEREAFTER. C/A: ACCOMPLISH FOLLOW UP INSPECTIONS PER ERA 631653-14AD, SECTION II , PRIOR TO 58,114 TFC AND EVERY 4,700 SDR ANCF20260309007None · noneOUTER WING REAR SPAR FWD FACE DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25SDR DALA2026030801596Fitting · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE REINFORCE FITTING LOCATED BTW FR 42 TO FR 43 AND -Y1292 TO -Y 1650.0 TORSION BOX LOWER SHELL IN MAIN WHEEL WELL (REFERENCE AA CARD 5100-01821- 01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAISDR DALA2026030801595Stringer · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED BTW FR 55 TO FR 58 IN AFT CARGO COMPARTMENT (REFERENCE AA CARD 5100-0182 1-01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED BTW FR 55 TO FR 58 IN AFT CARGO COMPARTMEN
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