JASC 5100
Service difficulty reports · 4,244
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 ABXA20211212128None · noneON TAXI OUT IT WAS FOUND THAT LOW SYSTEM HYDRAULIC PRESSURE LIGHT INOP, AIRCTAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RELAMPED & DIODE CARD CLEANED- IAW AMM 20-00-00 SYSTEM SERVICEABLE. AIRCRAFT RETURNED TO SERVICESDR A6WA202101178073Plate · corrodedREMOVED AND REPLACED 4 EACH BONDING PLATES P/N 601-37012-33. ***AIRCRAFT REMOVED FROM SERVICE*** RESTORED SURFACE FINISH. BOND CHECKED GOOD. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AWA SUPPLEMENT NO. 15-335 DATE OF ISSUE 12/22/2015. WORK PERFORMED UNDER ASDR CALA2021121002336Fitting · cracked(AD 2019-20-10) LH FR16 DOOR STOP FITTING #7 HAS CRACK INDICATIO NS ON I/B TOP HOLE AND I/B BOTTOM HOLE. REPAIR BEFORE NEXT FLIGH T.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN BFM ON NR# 0017169 G #7 FR16 LH IAW A319-5311-13-A2731 AND CSDR FDEA202112090121Frame Splice · unknownEVALUATE SUPPORT AT STA 1020, STR 5L & 5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W EA F-5310-T0366310 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIR.SDR FDEA202112090120Frame Splice · unknownEVALUATE SUPPORT AT STA 980, S-5L PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366306 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIRSDR FDEA202112090119Frame Splice · unknownEVALUATE SUPPORT AT STA 1100, S5L TO S-5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366309 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIRSDR R61A2022010500025Doubler · corroded**DURING HEAVY CHECK FOUND: CORROSION FOUND ON FLOOR SUPPORT AT LH SIDE BETWEEN FR 88 90. REPLACED FLOOR SUPPORT AT LH SIDE BETWEEN FR88 90 IAW SRM 51-41-01SDR R61A2022010500024Doubler · corroded**DURING HEAVY CHECK FOUND: CORROSION FOUND ON SPLICE AT LH SHEAR PANEL BETWEEN FR 87-88. REPLACED SPLICE IAW SRM 51-42-02SDR R61A2022010500023Doubler · corrodedCORROSION FOUND ON LH DOUBLER PLAE BETWEEN FR12-16. REPLACED DOUBLER PLATE IAW SRM 51-41-02SDR FDEA202112093074None · nonePERFORMED RTO AT 120 KIAS. CONSULTED QRH BRAKE COOLING CHART WHICH DIRECTED A 57 MINUTE BRAKE COOLING TIME. REF WRI 31-50 8385. PEFORMED HIGH ENERGY STOP INSP, SDR R61A2022010500026Door · corroded**DURING HEAVY CHECK FOUND: CORROSION FOUND ON WASTE DOOR SKIN PANEL BETWEEN FR88-89 BETWEEN STR 23-25 RH. REPLACED WASTE DOOR SKIN PANEL IAW SRM 51-41-02SDR FDEA202112052989None · damagedZONE 220 FLOOR BOARD 222AF IS DAMAGED. FABRICATED ZONE 220 FLOORBOARD 222AF ON VT MAE TRAVELER T21/1586160 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202112022979None · damagedZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1586162 IAW SRZ-25- 005 REVISION R. MAJOR REPAIRSDR FDEA202112022980None · damagedZONE 220 FLOOR BOARD 222MAF IS DAMGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1586164 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202112022978None · damagedZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON MAE TRAVELER T21/1586166 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202111302988Channel · corrodedCTR CARGO, L/H SIDE ROLLER TRAY EXFOLIATED AT APPROX STA. 1600 APPROX LBL 48. REMOVED AND REPLACED CENTER CARGO LEFT HAND ROLLER TRAY STA. 1600, LBL 48. REF MD11 SRM 51-30-01-0G, DWG AFJ7065.SDR MASA20211130594None · noneLH MAIN LANDING GEAR HYDRAULIC INTERFACE IN THE MLG BAY BETWEEN WS 14.50 AND WS 68.00 WAS FOUND WITH MISSING MATERIAL. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 20-2021-214.SDR MASA20211129582None · noneL/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 51-13-02, EA 69-2021-201.SDR MASA20211129581None · noneL/H WING LEADING EDGE SLAT NO. 2 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 69-2021-200.SDR DALA2026052703216None · noneESTABLISH MONITOR FRAME 60-61 ALONG STR 44 REQUIRES INSPECTION THIS REPAIR IS A CATEGORY B WITH SUBSEQUENT INSPECTIONS. ACCOMPLISHED INSPECTION REQUIREMENTS IAW A320 SRM 53-00-11 REPAIR WAS INSTALLED PER A320 SRM 53-00-11-300-029 AND AA 2335- 01033-05 ACCORDISDR R61A2021121601020Shear Angle · corrodedAT FRAME 88 BETWEEN STRINGERS 27R AND 28R SHEAR CLIP CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STGR 27R-28R REFER SRM 51-40-08.SDR FDEA202111222972None · damagedFOUND 20 4EA HOLES DRILLED AND UNUSED ON AFT PLATE BETWEEN STA 1681-1700 ON BL 0 THE DAMAGED SECTION OF THE AFT DECK PLATE WAS TRIMMED OUT PER SRM 51-10-02, THE AFT THECK PLATE WAS REPAIRED I.A.W EA # F-5310-T0365378 P1. THIS IS A MAJOR CATAGORY A REPAIRSDR FDEA202111222970None · corrodedFOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT STA 1681 LBL 40 TO RBL 40 UNDER SHEAR WEB THE FLOOR BEAM UPPER CHORD FWD FLANGE WAS REPAIRED WITH 2 ANGLES, 1 FILLER AND 1 STRAP P/N N918FD-NRC-N00352-01/-02/-03/-04 PER SRM 53-60-51, REPAIR 3, FIG. 201, DESDR ABXA20211119119Surge Valve · stickingDURING LEFT ENGINE START ONLY, DUCT PRESSURE GAUGE FLUCTUATIONS 10-30PSI AND ONLY ABLE TO ACHIEVE 16% N2 VERY SLOW TO SPOOL, NO PARAMETERS EXCEEDED. RT START NORMAL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED K10247 AND K10250, L SDR R61A2021120400983Doubler · corrodedCORROSION ON SKIN AFTER REMOVAL OF INTERCASOTAL, AREA OF HOT DRAIN MAST. REMOVED AND REPLACED INTERNAL HOT DRAIN MAST DOUBLER PER SRM 51-40-05SDR FDEA202111182973None · unknownFORWARD LOWER CARGO FLOOR,RIGHT HAND SIDE Z CHANNEL HAS A REPAIR SPLICE AT BS 710. REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA A DVI WAS PERFORMED PER SRM 51-10-08 AND THIS EXISTING REPAIR WAS FOUND IN SDR FDEA202111172889None · noneMAIN CABIN FLOOR PNL # 242 MCF HAS DENT DAMAGE TO UPPER SURFACE. FABRICATED ZONE 240 FLOOR BOARD 242 MCF ON VT MAE TRAVELER # T21/1584284 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202111172888None · damagedMAIN CABIN FLOOR PNL 242 MEF HAS PUNCTURE DAMAGE TO LOWER SURFACE AND DAMAGE TO LOWER CORNER STA 1020-TO-1055 BL0 TO 24 RBL. FABRICATED ZONE 240 FLOOR BOARD 242 MEF ON VT MAE TRAVELER # T21/1584285 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR CALA2021111802131Floor Support · corrodedFOUND CORROSION AT FLOOR STRUCTURE STA 328 RBL 55 REF AAR N/R 9637647 REMOVED CORROSION FOUND OUT OF LIMITS PER ECRA 5321-01330 REV B REMOVED DAMAGE AREA FROM FR328 RLB 55 AND INSTALLED REPAIR AS PER B737 SRM 53-10-51-2R-7 REPAIR 7 FIG 206 WORK ACCOMPLISHED BYSDR IPXA2021111676024None · noneINSPECTION TYPE:SEG4FOUND A DELAMINATED AREA ON THE UPPER SURFACE OF THE L/H O/B MAIN FLAP. LOCATED 31" IN FROM THE O/B SIDE OF THE PART, AND 8.5" UP FROM THE T/E. FOUND DURING INSP FOR E.O. B757-5750-36691-A.REPAIRED PANEL IAW B757 SRM 51-70-07-OG PER SRM 57-SDR JJBA20211115029None · noneBIRD STRIKE. PERFORMED SECTION 1: TEMPORARY REPAIR TO FWD FUSELAGE SKIN.SDR TSAA20211117025Skin · cracked1000582164 - REPAIRED CRACKS ON SKIN AT O/B CHORD@ B.S 727 LH STR 18L I.AW KF AEROSPACE DWG NO R27904.1-053-020-001 REV:NC AND BOEING PREVENTATIVE MOD SB 737-531166 REV 2 DATED JUNE
30,1994. AMOC ATTACHED.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 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 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 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 5
Back to JASC 5100