JASC 5500

Service difficulty reports · 490

Reports filed under 5500 · Empennage 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 = '5500'
  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.

SDR CALA2021101101851Skin · crackedEA 5510-01843 REV H CRACK NOTED ON L/H LOWER HORIZONTAL STAB SKI N AT RIB 8, STATION 147.9, IN BETWEEN PREVIOUS REPAIRS. (REF AAR NR 99911900) QC V935163). REMOVED DAMAGE CRACK & REPAIRED AREA ON L/H HORIZONTAL STAB LOWE R SKIN ALONG RIB 8 STATION 147.9 IN BETOct 11, 2021 · N37420 · Boeing 737924ERSDR P5CA2021093000370Channel · noneEMP - RH HORI STAB TIP FAIRING T/E SUPPORT CHANNEL 2 PLACES CRK(<P>REPLACE THE CRACKED CHANNEL IAW <SPAN>RI 55-10-14999.</SPAN></P>)Oct 9, 2021 · N858GT · Boeing 74787UFSDR SWAA2021101126618None · crackedLEFT HORIZONTAL FOWARD UPPER SLIDING SEAL CRACKED / R&R SLIDING SEAL PER MM REF-53-31-31AMT 21524INSP 50310Oct 5, 2021 · N8631A · Boeing 7378H4SDR CALA2021100601789Skin · crackedREF EA 5510-01843 REV H OP001 CRACK FOUND ON R/H HORIZONTAL STAB STA 129.50 I/B OF DRAIN HOLE CRACK LENGTH IS 0.375 REF AAR N/R 9633983 REQUIRED DETAIL VISUAL INSP 9000 F/C. EXTERNAL LOW FREQ EDDY CURRENT INSP 9000 F/C. INSPECTION THRESHOLD 56,000 TOTAL FLIGHTOct 5, 2021 · N39297 · Boeing 737824SDR CALA2021100601776Skin · crackedR/H HORIZONTAL STAB LOWER SKIN STAB SIA 120.30 HAS CRACK INDICAT REFERENCE FLEET CYCLE LOG PAGE 9783767. LOG PAGE FOR DIP ONLY INSTALLED REPAIR DOUBLER PER SRM 55-10-01-2R-11, SEE FLEET CYCLE ADDED LIMITS PER SRM 55-10-01-2R-11 PARA.5A. LOG PAGE 9783767 FOR DEOct 3, 2021 · N73291 · Boeing 737824SDR 7C7A2021100100018None · noneREPAIR FOR SCRATCH AND MULTIPLE DENT DAMAGE TO EMPENNAGE RH SIDE PANEL ASSEMBLY 85530007. REPAIRED IAW DEHAVILLAND RD8-55-3683 AND ECO 008.55-21.07.Oct 1, 2021 · N892EA · Dhav DHC8106SDR 2021FA0000275None · noneREPAIR FOR SCRATCH AND MULTIPLE DENT DAMAGE TO EMPENNAGE RH SIDE PANEL ASSEMBLY 85530007. REPAIRED IAW DEHAVILLAND RD8-55-3683 AND ECO 008.55-21.07.Oct 1, 2021 · N892EA · Dhav DHC8106SDR AALA202109301891Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON RIGHT HORIZONTAL STABILIZER (1 EA). REMOVED AND REPLACED ELEVATOR HINGE ARM NUMBER 4 ON RIGHT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.Sep 29, 2021 · N540UW · Airbus A321231SDR AALA202109303123Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 5 ELEVATOR ON RIGHT HORIZONTAL STABILIZER (1 EA). REMOVED AND REPLACED ELEVATOR HINGE ARM NUMBER 5 ON RIGHT HORIZONTAL STABILIZER (1EA) PER AMM 55-16-42-400-001-A.Sep 29, 2021 · N540UW · Airbus A321231SDR 2021FA0000268Skin · corrodedCORROSION ON LH VERTICAL STAB SKIN T/E BETWEEN MIDDLE AND LOWER HINGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ31657 DATED SEPTEMBER 26, 2021.Sep 29, 2021 · N507QS · Cessna 680ASDR SWAA2021110123901Rib · crackedCRACK DORSAL FIN RIB 8 AT STA 867 ACCESS PANEL 321A AT VERTICAL STABILIZER (1 EA) ; 2021-436125 / [01] REMOVED DORSAL FIN RIB 8 AT STA 867 ACCESS PANEL 321A AT VERTICAL STABILIZER AND 5EA FITTINGS AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND PERFORMED VISUALSep 27, 2021 · N420WN · Boeing 7377H4SDR CALA2021092801701Skin · crackedSUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AT STA 157.1 DETAILS REFER ATTACHED FIG. TRANSSFER REF NON- ROUTINE L/P 9130285 AND ORIGINA TED BY V897399 9,000 FLIGHT CYCLES THEREAFTER. CREATED DIP TO ACCOMPLISH SSep 27, 2021 · N34282 · Boeing 737824SDR CALA2021092801700Skin · crackedSUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK BETWEEN STA 92.7 AND 101.9 DETAIL REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130286 AND ORIGINATED BY V897399 9,000 FLIGHT CYCLES THEREAFTER. CREATED DIP TO ASep 27, 2021 · N34282 · Boeing 737824SDR CALA2021092801702Skin · crackedSUPPORT TASK EA 5510-01843 OP 1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AR STA 120.3 DETAILS REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130284 AND ORIGINAT ED BY V897399 INSPECTIONS AT 9,000 FLIGHT CYCLES THEREAFTER. CREATED DIP Sep 27, 2021 · N34282 · Boeing 737824SDR CALA2021092701698Panel · crackedSUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK BETWEEN STA 92.7 AND 101.9 DETAIL REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130286 AND ORIGINATED BY V897399 THIS ITEM WAS REPAIRED IAW SRM 55-10-01-2R-11 RESep 27, 2021 · N34282 · Boeing 7378SDR CALA2021092701690Panel · crackedSUPPORT TASK EA 5510-01843 OP 1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AR STA 120.3 DETAILS REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130284 AND ORIGINAT ED BY V897399 THIS ITEM WAS REPAIRED IAW SRM 55-10-01-2R-11 REPAIR 11 ANDSep 27, 2021 · N34282 · Boeing 7378SDR CALA2021092701689Panel · crackedSUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AT STA 157.1 DETAILS REFER ATTACHED FIG. TRANSSFER REF NON- ROUTINE L/P 9130285 AND ORIGINA TED BY V897399 THIS ITEM WAS REPAIRED IAW SRM 55-10-01-2R-11 REPAIR 11 ANDSep 27, 2021 · N34282 · Boeing 7378SDR SWIA202162718None · crackedRH VERTICAL STABILIZER 67.5% REAR SPAR DATUM APPROX DRAG ANGLE HAS POSSIBLE CRACK AS MARKED (C-CHECK RO 11-20-2021) REPAIRED THE RH FWD DRAG ANGLE FOR THE VERTICAL STABILIZER BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS REF CRJ700 SRM 5Sep 25, 2021 · N774SK · Cndair CL600*SDR SWAA2021110319934Mount · corrodedDORSAL FIN AFT RIGHT MOUNT HAS CORROSION ON FASTENERS. REMOVED AND REPLACED FASTENERS AT DORSAL FIN AFT RIGHT MOUNT REF B-737-700 SRM-51-40-02-0G-0.Sep 18, 2021 · N793SA · Boeing 7377H4SDR SWIA202162491None · crackedUPON FURTHER INSPECTION FOUND R/H AFT DRAG ANGLE JUST BELOW VERT. STAB. FS1220 - 67.5% CRACKED (MARKED) (C-CHECK RO 11/10/2021) REMOVED AND REPLACED THE RH AFT DRAG ANGLE ON THE VERT STAB FS1220 - 67.5% REF DRAWING AV670-21186 REV F, CRJ700 SRM 51-42-22-0Sep 16, 2021 · N772SK · Cndair CL600*SDR SWAA2021110919708Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION ; /Sep 16, 2021 · N783SW · Boeing 737*SDR SWAA2021110919702Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION ; /Sep 16, 2021 · N783SW · Boeing 737*SDR IXXA20211007064Skin Panel · delaminatedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT MAINTENANCE IDENTIFIED DELAMINATION ON THE UPPER LEFT HORIZONTAL STABILIZER SKIN PANEL LOCATED ON THE MOST INBOARD BONDED CORE SEGMENT OF THE INNER SKIN BETWEEN APPROXIMATELY AS STATION 240.701 AND Sep 10, 2021 · N791AX · Boeing 767281SDR CALA2021091001551Structure · corrodedPERFORM AN INSPECTION PER PART 2 OF THE LASTEST REVISION OF ECRA 5383-01003 ON OR BEFORE 50000 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM AN INSPECTION PER PART 2 OF THE LASTEST REVISION OF ECRA 5383-01003 ON OR BEFORE 50000 TOTAL AIRCRAFT FLIGHT CYCLES. REF LP 701Sep 10, 2021 · N17122 · Boeing 757224SDR SWIA202161812None · cracked*SUSPECTED CRACK ON THE V-STAB RH AFT DRAG ANGLE (C-CHECK RO 10/22/2021) REPAIRED V-STAB RH AFT DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.Aug 10, 2021 · N554CA · Cndair CL6002D24SDR SWIA202161202None · crackedL/H FWD DRAG ANGLE CRACK AT BASE OF VERTICAL STAB AT APPROX FS1181.00 (C-CHECK RO 9-21-21) REPAIRED LH FWD DRAG ANGLE AT VERTICAL STAB AT APPROX FS 1181.00 REF CRJ700 SRM 55-31-00-201-001-A01. NO NDT DEFECTS NOTED. LEAK CHECK AND TEST GOOD. COMPLIED WITH Aug 9, 2021 · N766SK · Cndair CL600*SDR SWIA202161698Damper · leakingLH ELEVATOR IB FLUTTER DAMPER IS LEAKING PISTON IS NOT SHOWING (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED SERVICEABLE L/H INBD ELEVATOR FLUTTER DAMPER IAW CRJ 200 AMM 27-34-05-400-801. REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Aug 5, 2021 · N932EV · Cndair CL6002B19SDR SWIA202161237Control Unit · failedL/H ELEVATOR HYD SYS #3 PCU FAILED FUNCTIONAL TEST OF THE PCU COMPENSATORS. (C-CHECK RO 9-21-21) REMOVED AND REPLACED L/H ELEVATOR #3 PCU REF CRJ 700 AMM 27-33-01-400-801-A01. OPS TEST GOOD, NO DEFECTS NOTED. COMPLIED WITH TASK CARD 27-320-1003-SKY.Jul 24, 2021 · N766SK · Cndair CL600*SDR SWIA202161236Control Unit · failedR/H ELEVATOR HYD SYS #1 PCU FAILED FUNCTIONAL TEST OF THE PCU COMPENSATORS. (C-CHECK RO 9-21-21) REMOVED AND REPLACED R/H ELEVATOR #1 PCU REF CRJ 700 AMM 27-33-01-400-801-A01. OPS TEST GOOD, NO DEFECTS NOTED. COMPLIED WITH TASK CARD 27-320-1003-SKY.Jul 24, 2021 · N766SK · Cndair CL600*SDR SWIA202161196None · cracked* RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE CRACKED (MARKED) (C-CHECK RO 9-21-21) REMOVED AND INSTALLED "NEW" R/H VERT STABILIZER AFT DRAG ANGLE AS REQ'D PER DRWG BA670-35002 REV. E, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-Jul 23, 2021 · N766SK · Cndair CL600*SDR IPXA2021071971814Elevator · puncturedINSPECTION TYPE:N/ADAMAGE REPORTED TO LEFT HAND INBOARD ELEVATOR PN 65B05700-17, .4 PUNCTURE THROUGH UPPER AND LOWER TRAILING EGDGE SKINSSANDED AREA AND REMOVED DAMAGE AT PUNCTURE AND REPAIRED PER EO B747-5520-80103-C.Jul 18, 2021 · N618UP · Boeing 7478FSDR CALA2021051000622Rib · damagedRH HORIZONTAL STABILIZER TIP DAMAGED REMOVED DAMAGED TIP CAP (348AR) REPLACED TIP ASSY. REF AMM 55-11-01-404-005 THROUGH ITEM F 1E, WILL ALSO NEED EDGE SEAL. ACCOMPLISHED AMM55-11-01-404-005 PAGE 2OF2 ITEM F (1) (F)&(H) ACCOMPLISHED EDGE SEAL AND INSTALLATION May 6, 2021 · N656UA · Boeing 767322SDR IPXA2021041068022Panel · crackedINSPECTION TYPE:SEGPANEL 341AL HAS A CRACK ON THE INTERNAL LOWER EDGECOMPLIED WITH EA 300-5741-27-A2570 AND UPS EO A300-5510-79893-AMar 13, 2021 · N129UP · Airbus A300F4622RSDR 2021FA0000076Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHT BELOW TOLERANCE AT LEFT ELEVATOR: HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G). WEIGHT HAS BEEN REPLMar 8, 2021 · N427QS · Emb EMB505SDR 2021FA0000064Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHT BELOW TOLERANCE AT LEFT ELEVATOR: HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G). WEIGHT HAS BEEN REPLFeb 26, 2021 · N437QS · Emb EMB505SDR JJBA20210209023Rudder · chafedRUDDER 1, LT SKIN CHAFFED 8 INCH FROM LOWER EDGE, 12 INCH LONG. CHAFFED LT SKIN OF RUDDER 1 AT LOWER EDGE REPAIRED.Feb 9, 2021 · N21129 · Emb EMB145XRSDR IPXA2021012865008Frame · crackedINSPECTION TYPE: 2C TAIL CONE FWD END RT CENTER GUIDE PIN FRAME IS CRACKED. REPAIRED TAIL CONE FRAME, IAW SRM 53-80-07 REPAIR 1. (MINOR)Jan 12, 2021 · N255UP · Doug MD11FSDR 2020FA0000523Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (7 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PADec 6, 2020 · N411QS · Emb EMB505SDR 2020FA0000512Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (7 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PANov 21, 2020 · N302QS · Emb EMB505SDR 2020FA0000511Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (15 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PNov 18, 2020 · N412QS · Emb EMB505SDR FDEA202009182243Intercostal · crackedEMPENNAGE,UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS,RIGHT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACKLINE FROM CORNER EDGE AT STATION Y=2164. RIGHT HAND SIDE LOWER WEB INTERCOSTAL REAR CENTER SPAR TO REAR SPAR CRACK AT STATION Y=2164 REPAIR CARRIED OUT, ASep 18, 2020 · N588FE · Doug MD11FSDR FDEA202009182242Intercostal · crackedEMPENNAGE, UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS, LEFT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACKLINE FROM CORNER EDGE AT STATION Y=2164. LEFT HAND SIDE LOWER WEB INTERCOSTAL REAR CENTER SPAR TO REAR SPAR CRACK AT STATION Y=2164 REPAIR CARRIED OUT, ASep 18, 2020 · N588FE · Doug MD11FSDR DALA2020080602719Attach Angle · crackedCRACK ON RH ATTACH ANGLE THROUGH ACCESS PANEL 370AL. NRC 00156: RH ATTACH ANGLE WAS REPLACED IAW DWG #5912188 REV BD AND MD-90 SRM 51-30-02 AND 51-30-05 VOL.II.Aug 5, 2020 · N963DN · Doug MD9030SDR 2020FA0000358Balance Weight · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE LEFT AILERON MASS BALANCE WEIGHT PART NUMBER PE915109-L31 WAS UNDER THE WEIGHT LIMITS (1761 GRAMS) AS PRESCRIBED BY THE SERVICE BULLETIN (MINIMUM 1787 GRAMS) -21 GRAMSAug 3, 2020 · N371QS · Emb EMB505SDR VNAA202007139992Angle · crackedRIGHT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE R/H VERTICAL STAB AFT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.Jul 13, 2020 · N572NN · Bombdr CL6002D15SDR 120B2020070800037Skin Panel · chafedEMPENAGE PANEL 148T3150-1 CHAFED.Jul 8, 2020 · N36NE · Boeing 767323SDR SWIA2020081151735Fairing · crackedLEFT UPPER STAB FAIRING 326AL WAS CRACKED. INSTALLED NEW PART.Jun 29, 2020 · N971SW · Cndair CL6002B19SDR VNAA202006019991Drag Angle · crackedREMOVED LT AFT DRAG ANGLE IAW SRM 51-42-10-001-001-A01, 51-42-24-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED THE LT AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.Jun 1, 2020 · N570NN · Cndair CL6002D24SDR 2020FA0000144Aneroid · mismanufacturedWE HAVE ORDERED 4 NEW PARTS FROM VARIOUS VENDORS AND WITH VARIOUS ORIGIN 8130-3S THAT ALL ARE NOT MEETING MANUFACTURER`S SPEC. THERE PARTS WERE ALL ORDERED BTW 10/5/18 AND 10/20/18. WE HAVE HAD THE PARTS IN QUESTION TESTED BY TWO INDEPENDENT VENDORS AS A 3RDFeb 12, 2020SDR 2020FA0000143Aneroid · mismanufacturedWE HAVE ORDERED 4 NEW PARTS FROM VARIOUS VENDORS AND WITH VARIOUS ORIGIN 8130-3S THAT ALL ARE NOT MEETING MANUFACTURER`S SPEC. THERE PARTS WERE ALL ORDERED BTW 10/5/18 AND 10/20/18. WE HAVE HAD THE PARTS IN QUESTION TESTED BY TWO INDEPENDENT VENDORS AS A 3RDFeb 12, 2020
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