JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer Structure, 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 = '5510' 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 = '5510' 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 AALA202205279582Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING WORN. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202205270955Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING WORN. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202205278236Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING WORN. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202205277935Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING WORN. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202205272131Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING WORN. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR SCNA20220526060Stabilator · crackedDEFECT: CRACK FOUND IN R/H HORIZONTAL STAB LWR INSPAR SKIN 134" FROM I/B EDGE AND 25" FROM L/E. RESOLUTION: REPAIRED R/H HORIZONTAL STABILIZER LOWER INSPAR SKIN 134" FROM I/B EDGE AND 25" FROM L/E IAW B737 SRM 55-10-01-2R-11 REV 75. REPAIR IS A CAT B. INSPSDR SCNA20220526059Stabilator · crackedDEFECT: REPAIRED RH HORIZONTAL STABILIZER LOWER INSPAR SKIN 98" FROM I/B EDGE AND 16" FROM L/E IAW SRM 55-10-01-2R-11 REV 75. REPAIR IS CAT B. INSPECTION THRESHOLD IS 56,000 TOTAL FLIGHT CYCLES PER SRM 55-10-01-2R-11 REV 75 TABLE 204.SDR SCNA20220526057Stabilator · crackedDEFECT: CRACKS FOUND IN R/H HORIZONTAL STAB LOWER INSPAR SKIN 39" FROM I/B EDGE, 19" FROM L/E AND 39" FROM I/B EDGE, 28" FROM L/E. RESOLUTION: REPAIRED R/H HORIZONTAL STABILIZER LOWER INSPAR SKKIN 39": FROM I/B EDGE, 19" AND 39" FROM L/E IAW SRM 55-10-01-2RSDR SWAA2022060707082Rib · crackedRH HORIZONTAL STABILIZER RIB# 5 STIFFENER 4 CRACK. CUT OUT DAMAGED AREA FROM VERTICAL STIFFENER PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG. 202.CUT OUT DAMAGED AREA AT WEB PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG. 202. PERFORMED HFEC AT CUT OUT IAW NDTM PSDR AALA202205188178Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT HORIZONTAL STABILIZER #2 ELEVATOR HINGE FITTING HAS BEARING WITH EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202205182127Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT HORIZONTAL STABILIZER #4 ELEVATOR HINGE FITTING HAS BEARING WITH EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42.SDR SWAA2022061606888Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. / [01] REMOVED DAMAGED PART FROM 3RD VERTICAL STIFFENER AND WEB IAW SRM 55-10-09-2R-4; STEP 4.B. FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 707SDR SWAA2022061606889Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 4TH VERTICAL STIFFENER IS CRACKED. / [01] REMOVED DAMAGED PART FROM 4TH VERTICAL STIFFENER AND WEB IAW SRM 55-10-09-2R-4; STEP 4.B.FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 707SDR SWAA2022051206505Rib · crackedRIB CHORD AT STA 105 IS CRACKED / [01] REMOVED AND REPLACED RIB CHORD IAW SRM 51-40-02SDR IXXA2022051302Floor Support · corrodedCORROSION FLOOR SUPPORT FS 1439 AT LBL8SDR R61A2022060400380Rib · crackedRH H-STAB SUSPECT CRACK AT RIB 11A & 12A BTWN FRONT SPAR & MID SPAR. R&R RIB 11A & 12A IAW TASK 170EO-55-10-0004_1.SDR SWAA2022053105996Skin · crackedLH HORIZONTAL STAB; LWR STAB SKIN CRACKED AT STAB STA 193.90; CUTOUT LOWER HORIZONTAL SKIN OF L/H HORIZONTAL STAB PER SRM 55-10-01-2R-11 STEP 4 (B) 2. AND DRILLED OUT EXISTING FASTENERS IN REPAIR AREA PER STEP 4 (F) 1. FABRICATED REPAIR DOUBLER PER SRM 55-10-0SDR SWAA2022060605341Support Angle · crackedRT HORIZONTAL STAB RIB 4 FOUND CRACK AT 'T' SUPPORT ANGLE / REMOVED FWD 'T' SUPPORT ANGLE AT RT HOR STAB INSPAR RIB #4 STA 120.30 AS PER B737-7 SRM 51-40-02.LOCATED AND OPENED NEW FASTENER HOLES AT NEW 'T' SUPPORT ANGLE STA 120.30 INSPAR RIB #4; FWD AREA.. AS SDR SWAA2022060804991Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.5; 3RD VERTICAL STIFFENER IS CRACKED. / REMOVED DAMAGE FROM 3RD VERTICAL STIFFENER OF THE RIB 129.5 IAW SRM 55-10-09-2R-4; STEP 4.B.(1); HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-0SDR SWAA2022050903879Skin · crackedRH HORIZONTAL STABILIZER LOWER SKIN IS CRACKED 1 LONG LOCATED 9.625 FWD OF AFT SPAR AT STAB STA 193.90 / [01] EA 22-155-01353 ISSUED.;[02] C/W EA 22-155-01353SDR SWAA2022060603537Rib · crackedRT HORIZONTAL STAB INSPAR RIB STA 120.10 (RIB 4 CRACK IN LOWER TRANSITION RADIOUS OF THE VERTICAL STIFFENER POSITION 4. / CRACK FOUND AT CUT OUT AREA OF STIFFENER #4 IAW NDTM PART 6; 51-00-00 PROCEDURE 23. LENGTH OF CRACK : 0.218' CUTOUT DAMAGED AT INSPAR RIBSDR SWAA2022060603538Rib · crackedRT HORIZONTAL STAB INSPAR RIB STA 120.10 (RIB 4 CRACK IN LOWER TRANSITION RADIOUS OF THE VERTICAL STIFFENER POSITION 2. / CUT AND REMOVED THE DAMAGE FROM THE VERTIAL STIFFENER OF THE RIB 4; AT RT HORIZONTAL STAB STA 120.10 ASPER B737-700 SRM 55-10-09-2R-4;PERFSDR ASAA2022050438349Skin · crackedL/H S-STAB LOWER SKIN HAS A CRACK LOCATED BETWEEN STAB STA. 129.50 AND 138.70 APROX. 1.5" LONG. CRACK LOCATION HAS BEEN MARKED AND ENDS OF CRACK HAVE BEEN MARKED. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB LOWER SKIN USING MAT .100 2024-T3 AND .071 2024-T3 PESDR SWAA2022061403033Rib · crackedRH HORIZONTAL STABILIZER;RIB 4 STAB STA 120.3;# 4 STIFFENER IS CRACKED. / [01] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER #4 OF THE RIB #4 FIG 202/ REPAIR 4 SHEET 1 IN IAW SRM 51-10-02-0G-0 AND 55-10-09-2R-4TRIMMED OUT DAMAGED HOLES AT LOWER CHORD SDR SWAA2022061403032Stiffener · crackedRH HORIOTAL STABILIZER RIB 4 STAB STA 120.3;#3 STIFFENER IS CRACKED. / CUT AND REMOVED THE DAMAGE FROM THE WEB AND MEASURED THE CORNER RADII OF THE WEB CUTOUT A MINIMUM OF 0.167' IN IAW SRM 51-10-02-0G-0 AND 55-10-09-2R-4;[02] PERFORMED HFEC INSP ON CUT OUT ARSDR AALA202206221333Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #1 ELEVATOR HINGE ARM FITTING HAS EXCESSIVE, PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR AALA202206226123Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #2 ELEVATOR HINGE ARM FITTING HAS EXCESSIVE, PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR AALA202206224427Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #3 ELEVATOR HINGE ARM FITTING HAS EXCESSIVE, PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR AALA202206224698Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #4 ELEVATOR HINGE ARM FITTING HAS EXCESSIVE, PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR AALA202206221700Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #5 ELEVATOR HINGE ARM FITTING HAS EXCESSIVE, PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR AALA202206222354Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #6 ELEVATOR HINGE ARM FITTING HAS EXCESSIVE, PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR SWAA2022061401678Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 ;17.5' FROM REAR SPAR ;I/B FASTENER ROW.CRACK LENGTH = 0.843' CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 17.5' FROM REAR SPAR I/B FASTENER ROW.CRACK LENGTH = 0.843' SDR SWAA2022053101500Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.100 INCH 2022-228134 / [01] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22. CALIPER SDR SWAA2022053101499Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.600 INCH 2022-228133 PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.7SDR SWAA2022053101665Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABALIZER LOWER SKIN STAB STA 193.90 ; 10' FROM REAR SPAR ; I/B FASTENER ROW. CRACK LENGTH = 1' CRACK FOUND AT RIGHT HORIONTAL STABALIER LOWER SKIN STAB STA 193.90 10' FROM REAR SPAR I/B FASTENER ROW. CRACK LENGTH = 1' . REMOVESDR SWAA2022053101691Rib · crackedCRACK INSPAR RIB STAB STA 101.90 AT 11 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-230716 / [01] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22;[02] REPAIRED INSPAR RIB STAB STA 101.90 AT 11 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW SRM SDR AALA202205104928Strap · brokenAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #2 HINGE ARM SAFETY STRAP TAB BROKEN. REPLACED HINGE ARM SAFETY STRAP PER SRM 51-42-11.SDR AALA202205025371Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND STABILIZER ELEVATOR #2 HINGE END FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202205027036Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND STABILIZER ELEVATOR #4 HINGE END FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.SDR FDEA202204261233Skin · dentedFOUND DENT ON HORIZONTAL STABILAIZER R/H SIDE LWR SKIN , SIZE : D=0.0231" L=2.79" W=2.46" PERFORMED HOT BOND REPAIR PER SRM 51-70-10,REPAIR 4,REF. SRM 55-10-01-1A,FIG. 101,DETAIL I,TABLE I,NOTE I. REP. DIM. : 5.5".REP. LOC. :56" FROM I/B AND 3.5" FROM AUXISDR SWAA2022053197530Seal · crackedR/H HORIZONTAL STAB I/B ACCESS PANEL 343AB HAS (1 EACH) METAL SEAL CRACKED. (18-040) / [01] REMOVED AND REPLACED DAMAGE METAL SEAL AT R/H HORIZONTAL STAB. ACCESS PANEL 343 AB; PER REF 737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR SWAA2022051897335Skin · crackedCRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 17' FROM FRONT SPAR I/B ROW. CRACK LENGTH 1'. CRACK FOUND AT LH HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 17' FROM FRONT SPAR I/B ROW. CRACK LENGTH 1'. / LOCATED AND DRILLED THE REPAIR HOSDR SWAA2022051897463Rib · crackedLT HORIZONTAL STABILIZER #4 RIB STIFFENER # 2 CRACKED / CUT AND REMOVED THE DAMAGE FROM THE WEB AT HORIZONTAL STABILIZER # 4 RIB STIFFENER #2 IN IAW SRM 51-10-02-0G-0 AND 55-10-09-2R-4 LOCATED AND DRILLED REPAIR PARTS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 ANSDR SWAA2022051897461Rib · crackedLT HORIZONTAL STABILIZER #4 RIB STIFFENER # 3 CRACKED. REMOVED DAMAGE AT LT HORIZONTAL STABILIZER #4 RIB STIFFENER #3 IAW SRM 51-10-02-0G-0 AND SRM 55-10-09-2R-4. VERIFIED STEP 1;PERFORMED HFEC INSP. ON RIB#4 STIFFENER #3 WEB IAW B737 NDT PART 6; 51-00-00; PROSDR SWAA2022051897462Rib · crackedLT HORIZONTAL STABILIZER #4 RIB STIFFENER # 4 CRACKED. REMOVED DAMAGE AT LT HORIZONTAL STABILIZER #4 RIB STIFFENER #4 IAW SRM 51-10-02-0G-0 AND SRM 55-10-09-2R-4. PERFORMED HFEC INSP. ON RIB#4 STIFFENER #2 WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACKSDR SWAA2022053196789Skin · crackedCRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.250 INCH 2022-206921 REPAIRED HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH SDR SWAA2022053196788Skin · crackedCRACK INDICATIONS FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.200 INCH 2022-206920 REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 ISDR SWAA2022051996041Skin Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 1.250 INCH. APPROX. 2022-211254 / REPAIRED LOWER EXTERNAL SKIN PANEL LOCATED ON LT HORIZONTAL STABILIZER LOWER SKIN PANSDR SWAA2022051996043Skin Panel · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 0.450 INCH. APPROX. 2022-211255 / REPAIRED LOWER EXTERNAL SKIN PANEL LOCATED ON RT HORIZONTAL STABILIZER AT STAB STA 19SDR CALA2022042101029Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 170.34, I/B ROW, 8" FROM FRONT SPAR , CRACK LENGHT : 0.947" REF. AAR NR:9649201 REQUIREMENTS INSPECTION THRESHOLD 56,000 TOTAL FLIGHT FLIGHT CYCLES EXTERNAL LOW FREQUENCY EDDY CURRENT (LFEC
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