# Service difficulty reports: N933AT

A list on [N933AT](https://openairdocs.org/aircraft/N933AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 176 reports

- [SDR DALA2026102305843](https://openairdocs.org/sdr/DALA2026102305843.md): Skin · cracked · Oct 22, 2026 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > FOUND A CRACK INDICATION COMMON TO ONE (1) HOLE ON THE LEADING EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER, COMPLIED WITH ER/A 613198-14. (1879346) (AIRCRAFT GROUNDED).
- [SDR DALA2026102305842](https://openairdocs.org/sdr/DALA2026102305842.md): Skin · cracked · Oct 22, 2026 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > FOUND CRACK ON VERTICAL STABILIZER RHS LEADING EDGE SKIN, COMPLIED WITH ER/A 613198-14. (1879339) (AIRCRAFT GROUNDED).
- [SDR DALA2026050502823](https://openairdocs.org/sdr/DALA2026050502823.md): Spar Cap · not reported · Apr 29, 2026 · N933AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > AMOC REQUIRED FOR ERA 583922-14AD REV B. AD 2018-10-08, VERTICAL STAB RH SPAR CAP. REPAIRED PER ER/A 00-583922. (1571590) (AIRCRAFT GROUNDED)
- [SDR DALA2026033002080](https://openairdocs.org/sdr/DALA2026033002080.md): Cap · cracked · Mar 27, 2026 · N933AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED CAP BS 1178, & LONG 17L, AFT ACCESORY COMPARTMENT. REPAIRED IAW PRI 632618-14. (1514424)
- [SDR DALA2026020900911](https://openairdocs.org/sdr/DALA2026020900911.md): Clamp · leaking · Feb 8, 2026 · N933AT · Boeing 717200 · APU Oil System
  > SMOKE AND ODOR IN CABIN, NO PASSENGERS ABOARD, ONLY CREW AND MTC. FOUND EXTERNAL LEAK AT TEE CLAMP BETWEEN GEARBOX AND INLET COMPRESSOR. OPENED PLENUM FOUND INLET CONTAMINATED WITH OIL. CLEANED CONTAMINATION FROM INLET PLENUM, R & R COALESCER BAGS IAW AMM
- [SDR DALA2025101407522](https://openairdocs.org/sdr/DALA2025101407522.md): Sensor · faulted · Oct 3, 2025 · N933AT · Boeing 717200 · Cabin Cooling System
  > ON THE GROUND ON APU POWER WHEN RT PACK TURNED ON, DID NOT COME ON. SMELLED SMOKE & THEN GOT PACK R FLO DISAG. TURNED SWITCH OFF AND SMELL WENT AWAY. R & R RT AIRFLOW SENSOR REF AMM 21-52. OPS CHK NML NO FAULTS, GOOD AIRFLOW. MEL/PLAC REMOVED. REVERSED M PR
- [SDR DALA2025082206252](https://openairdocs.org/sdr/DALA2025082206252.md): Not Reported · no discrepancy · Aug 16, 2025 · N933AT · Boeing 717200 · Standard Practices/Structures
  > WORKING REP CK RH MLG DOOR KEEL BEAM. C/W REP CK PER ER/A 621720-14 (9858048)
- [SDR DALA2025081806155](https://openairdocs.org/sdr/DALA2025081806155.md): Strut · discharged · Aug 13, 2025 · N933AT · Boeing 717200 · Nose/Tail Landing Gear Strut/Axle
  > ATB/GEAR- RETURNED ATL DUE TO PSEU FAIL MESSAGE WITH LANDING GEAR INDICATION INCORRECT. GEAR HANDLE UP AND INDICATION SHOWS DOWN. FAULT CLEARED WITH CORRECT INDICATION. RETURNED ATL PRECAUTIONARY. SERVICED NLG STRUT. REPLACED GEAR INDICATION BULBS. OPS NORMAL
- [SDR DALA2025040802706](https://openairdocs.org/sdr/DALA2025040802706.md): Defog System · faulted · Mar 29, 2025 · N933AT · Boeing 717200 · Windshield/Door Rain/Ice Removal
  > WHEN COCKPIT CREW TURNED ON THE WINSHIELD ANTI-FOG SWITCH, WHILE AT CRUISE, A SHOWER OF SPARKS SHOT OUT OF THE UPPER EDGE OF FIRST OFFICER'S FORWARD FACING WINDOW. THE CREW PULLED CIRCUIT BREAKER X26 10592. MAINTENANCE PERFORMED A VISUAL INSPECTION OF FIRST OF
- [SDR DALA2025021001047](https://openairdocs.org/sdr/DALA2025021001047.md): Lens · missing · Feb 9, 2025 · N933AT · Boeing 717200 · Emergency Lighting
  > THE FIRST EMERGENCY LIGHT ON CATWALK IN EMPENNAGE IS MISSING THE LENS COVER. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (LP #0803705)
- [SDR DALA2024041504429](https://openairdocs.org/sdr/DALA2024041504429.md): Lens · missing · Apr 13, 2024 · N933AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LENS COVER AT 17CDE MISSING. MAINTENANCE INSTALLED NEW EMERGENCY LENS COVER AT 17CDE PER B717 AMM 33-51. (LP #5874313)
- [SDR DALA2024041004264](https://openairdocs.org/sdr/DALA2024041004264.md): Union · leaking · Apr 10, 2024 · N933AT · Boeing 717200 · Hydraulic System, Main
  > AN EMERGENCY WAS DECLARED WITH ATC DUE TO THE RIGHT HYDRAULIC FLUID QUANTITY DECREASING. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOWN TEE ASSEMBLY. OPERATIONAL AND LEAK CHECKS WERE BOTH GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5300792)
- [SDR DALA2024030703129](https://openairdocs.org/sdr/DALA2024030703129.md): Skin · damaged · Mar 2, 2024 · N933AT · Boeing 717200 · Cargo/Baggage Doors
  > BOTTOM FWD CORNER OF AFT CARGO DOOR SKIN DAMAGED. REMOVED CARGO (AFT CARGO) PER B717 AMM 52-31. CUT OUT DAMAGE PER B717 SRM 52-00-01-2R. PERFORMED HFEC INSP OF CUT OUT REPAIR AREA PER B717 SRM 52-00-01-2R. NO CRACK INDICATION NOTED. COMPLETED REPAIR PER B717 S
- [SDR DALA2024022002324](https://openairdocs.org/sdr/DALA2024022002324.md): Skin · corroded · Feb 20, 2024 · N933AT · Boeing 717200 · Horizontal Stabilizer, Plate/Skin
  > A.D. RUST IN BARREL NUT AND CORROSION IN BARREL NUT HOLE (HSTAB SKIN) WAS FOUND IN NUT #11 AT RH HSTAB UPPER SIDE, IN REFERENCE NRC 438. SUMMARY OF NRC 00727: HORIZONTAL STABILIZER RH UPPER BARREL NUT HOLE #11 AND LOWER BARREL NUT HOLE #29 WERE REPAIRED PER PR
- [SDR DALA2024021502203](https://openairdocs.org/sdr/DALA2024021502203.md): Angle · cracked · Feb 14, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ANGLE STA 710-715 X=-43 AT CENTER TANK WING UPPER SURFACE AT PAX CABIN (WINGBOX AREA). SUMMARY OF NRC 00320: ANGLE STA 710-715 X=-43 AT CENTER TANK WING UPPER SURFACE AT PAXCABIN WAS REPAIRED PER PRI 615191-14 REV 4 AND ERA 615191-14 REV ORIGINAL, SECTIO
- [SDR DALA2024021502202](https://openairdocs.org/sdr/DALA2024021502202.md): Beam · cracked · Feb 14, 2024 · N933AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKS ON BEAM #1 FWD AND AFT EDGE (INTERNAL STRUCTURE) AT PASSENGER DOOR (L1). SUMMARY OF NRC 00083: BEAM #1 FWD AND AFT EDGE (INTERNAL STRUCTURE) AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7. (LP #0201880)
- [SDR DALA2024021402123](https://openairdocs.org/sdr/DALA2024021402123.md): Unknown · damaged · Feb 14, 2024 · N933AT · Boeing 717200 · Rudder Structure
  > ELONGATED HOLES ON AREA TO ATTACH ANCHOR NUT ON SETTLEMENT AREAS OF ACCESS 370CR AT RUDDER LOWER AREA. SUMMARY OF NRC 00455: AREA TO ATTACH ANCHOR NUT ON SETTLEMENT AREAS OF ACCESS 370CR AT RUDDER LOWER AREA WAS REPAIRED PER ERA 615547-14, REV ORIGINAL. MAINTE
- [SDR DALA2024021402122](https://openairdocs.org/sdr/DALA2024021402122.md): Pan · worn · Feb 14, 2024 · N933AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR ON EXTERNAL PAN UPPER FWD/AFT CORNERS AT AFT CARGO DOOR. SUMMARY OF NRC 00116: EXTERNAL PAN UPPER FWD CORNER AT AFT CARGO DOOR WAS BLENDED OUT AND MEASURED AS FOLLOW: ORIGINAL THICKNESS OF 0.050" REMAINING THICKNESS.0.048" THEREFORE IT IS WITHIN THE ALLOW
- [SDR DALA2024021201855](https://openairdocs.org/sdr/DALA2024021201855.md): Skin · dented · Feb 9, 2024 · N933AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS ON RH FWD MOVABLE FLAP. SUMMARY OF NRC 00381: DENTS (10 LOCATIONS) ON RH FWD MOVABLE FLAP, #2, #3, #5, #6, #8, #9, & # 10 WERE EVALUATED AND FOUND TO BE WITHIN LIMTS PER B717-200 SRM 57-53-01-1A-1 PAR 3 A (1)(2)(4). DENT #1: O/B=18 IN, T/E=6.700 IN, L=1.
- [SDR DALA2024020901764](https://openairdocs.org/sdr/DALA2024020901764.md): Frame · cracked · Feb 9, 2024 · N933AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON RH FRAME STA 1037 LONG 14RH AT PAX CABIN. SUMMARY OF NRC 00296: CRACK ON RH FRAME STA 1037 LONG 14RH AT PAX CABIN WAS REPAIRED PER PRI 614871-14 REV 2 AND ERA 614871-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614871 ADDED FOR AC 9
- [SDR DALA2024020901763](https://openairdocs.org/sdr/DALA2024020901763.md): Cap · cracked · Feb 8, 2024 · N933AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON CAP STA 1022 AND LONG 1. SUMMARY OF NRC 00351: CAP STA 1022 AND LONG 1 WAS REPAIRED PER PRI 615124-14 REV 0 AND ERA 615124-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615124 ADDED FOR AC 9566. (LP #0192767)
- [SDR DALA2024020801687](https://openairdocs.org/sdr/DALA2024020801687.md): Skin · cracked · Feb 8, 2024 · N933AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 0514: CRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. WERE REPAIRED PER PRI 614977-14
- [SDR DALA2024020801686](https://openairdocs.org/sdr/DALA2024020801686.md): Skin · cracked · Feb 7, 2024 · N933AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00513: FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER PRI 614985-14 REV 3 AND ERA 614985-14 REV ORIGINAL SECTION I: PERMANENT
- [SDR DALA2024020801684](https://openairdocs.org/sdr/DALA2024020801684.md): Frame · cracked · Feb 6, 2024 · N933AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CANTED FRAME INTERNAL STRUCTURE Y=1200 REF STGR 17 APROX. SUMMARY OF NRC 00257: CANTED FRAME INTERNAL STRUCTURE Y=1200 REF STGR 17 APROX WAS REPAIRED PER PRI 614980-14 REV 1 AND ERA 614980-14 REV ORIGINAL.
- [SDR DALA2024020601579](https://openairdocs.org/sdr/DALA2024020601579.md): Frame · cracked · Feb 6, 2024 · N933AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAMES 2 EA, STA Y=660 AND 675 OUTBOARD EDGE LH SIDE OF KEEL BEAM AREA. SUMMARY OF NRC 0807: FRAME STA=660 AND FRAME STA=675 OUTBOARD EDGE LH SIDE OF KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND 51-70-11-2R PROC 1 REPAIR
- [SDR DALA2024020601577](https://openairdocs.org/sdr/DALA2024020601577.md): Pan · cracked · Feb 4, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERNAL PAN FWD EDGE ON BEAM #1 AT FWD CARGO DOOR. SUMMARY OF NRC 00103: INTERNAL PAN FWD EDGE ON BEAM #1 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0187095)
- [SDR DALA2024020601576](https://openairdocs.org/sdr/DALA2024020601576.md): Doubler · cracked · Feb 4, 2024 · N933AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON INTERNAL DOUBLER AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR. SUMMARY OF NRC 00104: INTERNAL DOUBLER (WEB) AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER BOEING DWG 9957664 REV "N", B717-200 SRM 51-41-01-0G, 51-41-02-0
- [SDR DALA2024022102376](https://openairdocs.org/sdr/DALA2024022102376.md): Drag Brace · corroded · Feb 3, 2024 · N933AT · Boeing 717200 · Nose/Tail Landing Gear
  > CORROSION ON DRAG BRACE BORE (LH TAPER PIN HOLE) AND CORROSION ON LH / RH (2 EA) TAPER PIN AT NLG. DRAG BRACE WAS REMOVED PER B717-200 AMM 32-22-05 000-802. SUMMARY OF NRC 00250: NLG DRAG BRACE ASSY WAS REPLACED PER B717-200 AMM 32-22-05. OPERATIONAL TEST OK.
- [SDR DALA2024020601575](https://openairdocs.org/sdr/DALA2024020601575.md): Pan · cracked · Feb 3, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LOWER EDGE OF EXTERNAL PAN AT FWD CARGO DOOR WAS FOUND IN REF NRC 00098. SUMMARY OF NRC 00788P: LOWER EDGE OF EXTERNAL PAN AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0185876)
- [SDR DALA2024020601574](https://openairdocs.org/sdr/DALA2024020601574.md): Frame · cracked · Feb 3, 2024 · N933AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME STA 696 RH AT PAX CABIN. SUMMARY OF NRC 00462: CRACKED FRAME TAB OF THE OVERWING FRAME STA 696 RH AT PAX CABIN WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND 51-41-02-0G IN REFERENCE CARD 5310-01436-
- [SDR DALA2024020601572](https://openairdocs.org/sdr/DALA2024020601572.md): Intercostal · cracked · Feb 3, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL BTW BEAMS 4 AND 5 STA Y=180 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00087: INTERCOSTAL BTW BEAMS 4 AND 5 STA Y=180 AT PASSENGER DOOR (L1) WAS FABRICATED AND REPLACED PER DWG 9955763 REV K, B717-200 SRM 51-41-01-0G AND 51-41- 02-0G. (LP #018
- [SDR DALA2024020301507](https://openairdocs.org/sdr/DALA2024020301507.md): Beam · cracked · Feb 1, 2024 · N933AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK BEAM NBR 6 (MID SECTION) ON PASSENGER DOOR (L1). SUMMARY OF NRC 00174: BEAM NBR 6 (MID SECTION) ON PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 51-70-11-2R, PROCEDURE 1, REPAIR 1. (LP #0182665)
- [SDR DALA2024012901219](https://openairdocs.org/sdr/DALA2024012901219.md): Fitting · cracked · Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACK ON VERTICAL FITTING ON AFT PRESSURE BULKHEAD STA 1053 LONGERON #1 (ABOVE DOOR CUT OUT) AT PAX CABIN. SUMMARY OF NRC 00522: SPRING OF THE ARM ASSEMBLY WAS REMOVED AND INSTALLED PER B717-200 AMM 53-52-02-020-801 AND 53-52-02- 420-801, VERTICAL FITTING ON A
- [SDR DALA2024012601171](https://openairdocs.org/sdr/DALA2024012601171.md): Cusp Web · corroded · Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON DOUBLER OF LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB. SUMMARY OF NRC 00477: CORROSION LEVEL 2. DOUBLER OF REPAIR ON LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB WAS REPLACED PER B-717-200 SRM 53-00-55-2R. (LP #0171752)
- [SDR DALA2024012501107](https://openairdocs.org/sdr/DALA2024012501107.md): Cusp Web · corroded · Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN. SUMMARY OF NRC 00510: CORROSION LEVEL 2. AREA ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R. (LP #0170434)
- [SDR DALA2024012501106](https://openairdocs.org/sdr/DALA2024012501106.md): Frame · cracked · Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON LH FRAME STA 1037 LONG 17LH AT PAX CABIN. SUMMARY OF NRC 00294: LH FRAME STA 1037 LONG 17LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R. (LP #0170333)
- [SDR DALA2024011900806](https://openairdocs.org/sdr/DALA2024011900806.md): Cusp Web · cracked · Jan 18, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN. SUMMARY OF NRC 00376: CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 51-41-02-0G AND 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0160778)
- [SDR DALA2024010900328](https://openairdocs.org/sdr/DALA2024010900328.md): Unknown · unknown · Jan 8, 2024 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON REPAIR PLUG ON OUTB SEAT TRACK X=56 LH IN STA Y= 547 AND 610 (2 EA). SUMMARY OF NRC 00604: CORROSION LEVEL 2. PLUG ON OUTB SEAT TRACK X=56 LH IN STA Y=547 AND 610 (2 EA) WERE REPLACED PER B-717-200 SRM 51-41-01-0G AND 53-20-52-2R-1 REPAIR 1. (LP #
- [SDR DALA2024010500203](https://openairdocs.org/sdr/DALA2024010500203.md): Unknown · unknown · Nov 23, 2023 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- A SKIN LAYER CRACK WAS FOUND ON THE LEADING-EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER OF A B717-200. THE CRACK WAS REPAIRED PER ER/A 613198-14. THIS ER/A REQUIRES FOLLOW ON INSPECTION. UPDATED MONITOR LOG THRESHOLD TO ACCOUNT FOR TIME FLOWN SINCE SE
- [SDR DALA2023112009531](https://openairdocs.org/sdr/DALA2023112009531.md): Unknown · unknown · Nov 18, 2023 · N933AT · Boeing 717200 · Emergency Lighting
  > ALL TAIL COMPARTMENT EMERGENCY PATHWAY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-260 & B5-116 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4368053)
- [SDR DALA2023103008882](https://openairdocs.org/sdr/DALA2023103008882.md): Unknown · unknown · Oct 30, 2023 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > FOUR (4) CRACK INDICATIONS NOTED ON RT VERT STAB (MARKED) REF STEP 12 OF AMDS CARD 5530-01048-02 (AD2018-10-08). AFTER SEPERATION OF LAYERS PER AMDS 5530-01048-02, BHEC INSP SHOWS UPPER 3 HOLES OK AND LOWER MARKED HOLE HAS CRACK IN SKIN LAYER ONLY (QC 4031). C
- [SDR DALA2023112809766](https://openairdocs.org/sdr/DALA2023112809766.md): Unknown · unknown · Oct 29, 2023 · N933AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > AD RELATED. DTE ERA 613198-14 REV ORIGINAL. ERA ISSUED FOR VERT STAB FRONT SPAR REPAIR AT ZFS=43.000, RHS. DAMAGE TOLERANCE EVALUATION REQUIRED ADDL TIME RLTD MON #0078171. DAMAGE TOLERANCE EVALUATION REQUIRED. DTE LOG #0040724 NO LONGER LIMITED TO 30 DAYS. ER
- [SDR DALA2023021401130](https://openairdocs.org/sdr/DALA2023021401130.md): Unknown · unknown · Feb 6, 2023 · N933AT · Boeing 717200 · Fuselage Floor Panel
  > AFT LOWER CARGO COMPARTMENT LINERS METAL TRANSITION STRIP BENT UP. MCC FCP DEFERRAL TO MEL 25-50-01, FLIGHT CREW PLACARD INSTALLED. LOWER COMPARTMENT LINERS BINS 3-4. INSTALLED SIDEWALL PANELS PUSHED OUT. FOUND PNL 181HF BENT UP AND WILL NEED REPLACED REF IPC
- [SDR DALA2023011200228](https://openairdocs.org/sdr/DALA2023011200228.md): Light · inoperative · Jan 11, 2023 · N933AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR EMERGENCY LIGHTS WERE ON IN THE ARM POSITION AT WAKE UP. MAINTENANCE REPLACED THE EMERGENCY LIGHTS RACK PER B717 AMM 33-51. OPERATIONAL CHECK IS OK. (LP #9624134)
- [SDR DALA2022120607806](https://openairdocs.org/sdr/DALA2022120607806.md): Slide · failed · Dec 4, 2022 · N933AT · Boeing 717200 · Escape Slide
  > CATERING ATTEMPTED TO OPEN 1L WITHOUT VISUAL CONFIRMATION FROM LEAD FA, AFTER JET WAY PULLED AND DOORS ARMED. THE RAFT FELL AND DID NOT INFLATE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE SL
- [SDR DALA2022102606954](https://openairdocs.org/sdr/DALA2022102606954.md): Battery · inoperative · Oct 22, 2022 · N933AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHTS TO NOT BE TESTING PROPERLY. THE OVERWING EMERGENCY EVACUATION BATTERY WAS REPLACED PER B717 AMM 33-51. (LP #9586900)
- [SDR DALA2022082205657](https://openairdocs.org/sdr/DALA2022082205657.md): None · none · Aug 19, 2022 · N933AT · Boeing 717200 · Elevator, Plate/Skin
  > ON WALKAROUND FOUND MISSING PANEL ON UNDERSIDE OF LEFT HAND ELEVATOR. MAINTENANCE INSTALLED A NEW PANEL PER AMM 06-33 B717. (LP #9236464)
- [SDR DALA2022051003226](https://openairdocs.org/sdr/DALA2022051003226.md): Frame · corroded · May 8, 2022 · N933AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FRAME CHANNEL STA Y=889 BTW LONG 29LH AND 29 RH AT AFT CARGO COMPARTMENT IN REF NRC 00107. SUMMARY OF NRC 00214: CORROSION LEVEL 2, FRAME WAS REPAIRED PER B717 SRM 53-20-07-2R, REPAIR 3. PERFORM A VISUAL INSPECTION, INITIAL AT 25,000 FH AND REPETI
- [SDR DALA2022050603162](https://openairdocs.org/sdr/DALA2022050603162.md): Skin Panel · cracked · May 5, 2022 · N933AT · Boeing 717200 · Wing, Plate/Skin
  > CRACKED UPPER SKIN PANEL TRAILING EDGE STA XRS 111.500 AT LH WING (LW). SUMMARY OF NRC 00030: CRACKED UPPER SKIN PANEL TRAILING EDGE STA XRS 111.500 AT LH WING WAS REPAIRED PER. PRI 599039-14 REV. 0 AND ER/A 599039-14, REV. ORIGINAL, SECTION I: PERMANENT REPAI
- [SDR DALA2022050503142](https://openairdocs.org/sdr/DALA2022050503142.md): Channel · corroded · May 4, 2022 · N933AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT. SUMMARY OF NRC 00113: CORROSION LEVEL 2, FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT, WAS REPAIRED PER B717-200 SRM 53-20-07-2R, REPAIR 3. (LP #2223147)

Next page: https://openairdocs.org/aircraft/N933AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 n_number = 'N933AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N933AT/reports

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