JASC 5512
Service difficulty reports · 7,887
Reports filed under 5512 · Horizontal Stabilizer, Plate/Skin, 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 = '5512' 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 = '5512' 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 SWAA094883Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA200907282811Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 35R BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO LIMITATIONS. REPAIRED AS PER EA 1-5510-131624, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 107SDR FDEA200907282810Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 34R BARREL NUT BORE SIDEWALL BEARING SURFACE CORROSION REWORKED. FOUND EXCEEDED EO LIMITATIONS. REPAIRED AS PER E.A. 1-5510-131624, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR DLM88091254Skin · crackedRIGHT UPPER AFT STABILIZER SKIN CRACKED. C/W ERA 460477-14 REV A CODE 9-55-11. PERM REPAIR RT HORIZ STAB / UPPER AFT SKIN PNL / INBOAD END CRACK ON NR 1 EO CARDS 1-3 09-460214-12AD REV D ME 08.SDR DU4R2009389Skin · dentedDENT ON RT HORIZ STAB UPPER SURFACE SKIN 8 INCHES FROM FWD SPAR AND 80 INCHES FROM INBD END.SDR C2XA09SH210Skin · corrodedSHV - DURING C-CHECK LT HORIZONTAL L/E UPPER AND LOWER SURFACE HAS CORROSION AROUND ALL RIVET HEADS AND SCREW HEADS. MAINTENANCE REMOVED CORROSION BY POLISHING LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SURFACES IAW EC5530-01116. THE AIRCRAFT WAS APPROVED SDR SWAA094563Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.SDR DLM88091200Skin · crackedCRACK IN STAB UPPER AFT RT SKIN. REPAIRED SKIN IN ACCORDANCE WITH ERA 460409-14AD.SDR CALA2009071300368Skin · crackedLEFT HORIZONTAL STAB LOWER INSPAR SKIN INSPECTION FAILED AT STAB STA 129.50. DETECTED 2 CRACKS (1) MOST FWD 1.25 INCH IN LENGTH (2) 6 INCHES AFT OF (1) CRACK LENGTH IS 1 INCH. INSTALLED INTERIM REPAIR IAW EC/RA 5510-02028. DIP INITIATED TO ACCOMPLISH AN INITSDR DLM88091413Skin · crackedRIGHT HORIZ STAB UPPER AFT SKIN PANEL / INBOARD END CRACKED. SKIN REPLACED IAW ER/A 460410-14AD REV B ON PEMCO PD 1000-3 ROUTINE 1792R840.SDR DLM88091101Skin · crackedRT STAB UPPER AFT SKIN CRACKED. REPLACED UPPER AFT RT STAB SKINSDR SWAA094286Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED AT 101.90. REPAIRED SKIN PER SRM.SDR SWAA094285Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED AT 101.90. REPAIRED SKIN PER SRM.SDR FDEA200906302391Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK NR 16L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA 1-5510-131623, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302390Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT 1: HOR STAB LT UPPER PLANK NR 06L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW NR 1-5510-131625, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302389Skin · corrodedEO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK, NR24L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA NR1-5510-131623, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR SWAA094223Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.SDR SWAA094222Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.SDR SWAA094221Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.SDR ASAA0976009Skin · crackedLT H STAB SURFACE SKIN HAS EVIDENCE OF A CRACK LOCATED 72 DU FM IB END 17IN FROM AFT EDGE OF STAB LE SKIN. STEP DRILLED CRACKED INSTALLED REPAIR DOUBLER.SDR AALA20090623TUL06Skin · gougedLEFT HORIZONTAL STAB LOWER SKIN GOUGED STATION 191 APPROXIMATELY 6 INCHES AFT OF FRONT SPAR. INSTALLED DOUBLER PER SRM 55-10-01-2R.SDR AALA20090623TUL05Skin · gougedLEFT HORIZONTAL STAB LOWER SKIN GOUGED AT STATION 209 APPROXIMATELY 11 INCHES AFT OF FRONT SPAR. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 55-10-01-2R.SDR WRLA2009171Skin · gougedDURING C-CHK IN RME INSP/MX FOUND LT HORIZONTAL I/B LEADING EDGE SKIN GOUGED. MEASURED GOUGE AND FOUND TO BE OUT OF LIMITS. REMOVED L/E SEGMENT. REMOVED DAMAGE AND REPAIRED. REINSTALLED L/E SEGMENT. ALL WORK DONE IAW DC-10 SRM 55-00-01 & 55-20-01.SDR ASAA0995962Skin · dentedDENT IN LT HORIZONTAL STAB LEADING EDGE AT RIB LOCATED 6 INCHES OUTBOARD OF OUTBOARD LEADING EDGE SEAM. REMOVED AND REPLACED WITH SERVICEABLE LEADING EDGE ASSY.SDR FDEA200906122044Skin · crackedDURING INSP OF COSTANT SECTION STB, FOUND UP PANEL, INSP POSITION 3, WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-129688.SDR ASAA0995978Skin · crackedLT HORIZONTAL STAB IS CRACKED AT STAB STA 129.5, 9 INCHES AFT OF FRONT SPR LOWER SKIN. REPAIRED IAW EA.SDR ASAA0995976Skin · crackedLT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB. STA 128 17 INCH AFT OF FRONT SPAR. REPAIRED IAW EA.SDR DLM88091015Skin · crackedHORIZONTAL STAB UPPER RT AFT SKIN CRACK ERA 460327-14AD. C/W PERMANENT REPAIR. REPLACED UPPER AFT SKIN PANEL PER EA 09-460214-12 REV D ME08.SDR CALA2009060100286Skin · crackedLOWER SURFACE OF RIGHT HORIZONTAL STAB SKIN IS CRACKED APPROXIMATELY 24 INCHES FROM FWD SPAR AND RIB STA 129.5. REPAIRED CRACK PER ECRA 5510-02012.SDR CALA2009060100285Skin · crackedCRACK ON LOWER SURFACE OF RIGHT HORIZONTAL STAB 18 INCHES FROM FWD SPAR AND AT STA 129.5. REPAIRED CRACK PER ECRA 5510-02012.SDR FDEA200905281836Skin · crackedDURING INSP OF HORIZ STAB CONSTANT AND OUTER SECTIONS SKIN PANEL, FOUND PANEL P/N 7228-1, P/N 7280-2, P/N 7278-2 WITH CRACK, ACCOMPLISHED EA NR 8-5510-129682.SDR USAA2009052891319Skin · crackedCLT - C5 - MAJOR REPAIR - NR 03C70955008/001 - CRACK ON RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN FORWARD OF REAR SPAR BALANCE PANEL 0049. REPAIRED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN IAW US AIRWAYS TYPICAL REPAIR 55-10-07 REV "D".SDR ASAA0995697Skin · crackedLT HORIZONTAL STABILIZER LOWER SURFACE IS CRACKED. REPAIRED IAW EA 900 55EA 01352SDR SWAA093322Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.SDR CALA2009051900267Skin · crackedSUPPORT TASK LT HORIZONTAL STAB LWR SKIN CRACKED TWO PLACES AT STA 129.5 REPAIRED LWR SKIN ON LT HORZ-STAB AT STA 129.5 REF ECRA5510-02 009 AND INITIATE A DIP 094125 TO READ AS FOLLOW: ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM 18-MAY-2009 PER ECRA55SDR IPXA09855876Skin · dentedINSPECTION TYPE:SV SURVEY SEQ 852-SI-05 LT HORIZ STAB L/E DENTED AT REPAIR AT STA XFS 91-2 50. REPAIR ACCOMPLISHED PER DC8-SRM 55-2-1 FIG 4 TR 55-2.SDR ASAA0995637Skin · dentedLT HORIZONTAL STAB L/E IS DENTED STAB STA 104. FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS DOUBLER.SDR ASAA0995636Skin · dentedLT HORIZONTAL STAB L/E IS DENTED. DENT OUT OF LIMITS TRIMMED OUT DAMAGE FABRICATED AND INSTALLED DOUBLER.SDR 2009FA0000404Skin Panel · debondedDURING THE SID INSP, WITH THE HORIZONTAL STABILIZER REMOVED, DEBONDING WAS FOUND USING ULTRASOUND INSP ON THE BOTTOM CENTER WHERE THE LT AND RT PANELS ARE JOINED TOGETHER WITH FINGER DOUBLERS.SDR 2009FA0000399Skin · debondedDURING THE SID INSP OF THE REMOVED HORIZONTAL STABILIZER, AREAS OF DIS-BOND WERE FOUND ON THE BOTTOM NEAR THE CENTER OF THE STABILIZER. IAW MFG, THIS IS A CRITICAL AREA OF THE HORIZONTAL STABILIZER.SDR CALA2009051400247Skin · crackedRT HORIZONTAL STAB LWR SKIN HAS CRACK LOCATED AT STA 129.5 AND 24 INCHES AFT OF FWD SPAR (B737-55-3-0251). SEE BLOCK 38 FOR PARTIAL WORK ACCOMPLISHED. INSTALLED REPAIR DOUBLER REF ECRA 5510-02004. SEE LOG 9706715 AND LOG 97068 85 FOR DIP 93950.SDR C2XA09SH146Skin · corrodedSHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED LT HORIZONTAL STABILIZER LEADING EDGE IAW EMB-145 EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH147Skin · corrodedSHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED RT HORIZONTAL STAB LEADING EDGE IAW EMB-145 EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA092714Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT REAR SPAR STAB STA 125. REPAIRED SKIN PER SWA EA.SDR FDEA200904271424Skin · crackedDURING INSPECTION OF HORIZONTAL STABILIZER CONSTANT AND CUTER SECTION SKIN PANELS FOUND NR 3 PANELS WITH CRACKS. REPAIRED AREA IAW EA NR 8-5510-126253 AND EA NR 8-5510-126254.SDR USAA2009050891120Hinge Pin · corrodedSAL - C19 - MAJOR REPAIR - CORROSION ON OUTER STABILIZER HINGE PIN, LEFT SIDE CENTER SECTION HINGE. REPLACED OUTER STABILIZER HINGE PIN, LEFT SIDE CENTER SECTION HINGE IAW B737 AMM 27-41-31-4.SDR ASAA0945306Skin · crackedLT HORZ STAB LWR SKIN CRACKED (NDI VERIFIED 2 INCH CRACK) STAB STA 125 REAR SPAR AREA. REPAIRED IAW EA 400-55EA-01247.SDR USAA2009050891121Web · crackedSAL - C19 - MAJOR REPAIR - CRACK ON WEB AT HORIZONTAL STABILIZER CENTER SECTION BETWEEN STA 1088 & STA 1104 LBL 22. REPAIRED WEB AT HORIZONTAL STABILIZER CENTER SECTION BETWEEN STA 1088 & STA 1104 LBL 22 IAW B737 SRM 51-70-13.SDR SWAA092586Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND LT STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.SDR ASAA0945258Skin · misrepairedPREVIOUS REPAIR LT HORIZONTAL L/E IMPROPER STA 220 226. REMOVE EXISTING REPAIR, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR IAW B737 400 SRM 55 10 01.
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