# Service difficulty reports: N794AJ

A list on [N794AJ](https://openairdocs.org/aircraft/N794AJ.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 2 · 62 reports

- [SDR FXGA07312024001](https://openairdocs.org/sdr/FXGA07312024001.md): Hose · leaking · Jul 27, 2024 · N794AJ · Boeing 727227 · Hydraulic System, Main
  > ON DESCENT "A" SYSTEM HYDRAULIC QUANTITY FLUID STARTED DECREASING. FOUND LEAK FROM HOSE FITTING ON #2 SPOILER ACTUATOR. REPLACED ORING ON FITTING
- [SDR FXGA202307122336](https://openairdocs.org/sdr/FXGA202307122336.md): Unknown · unknown · Jul 12, 2023 · N794AJ · Boeing 727200 · Fuselage Structure (General)
  > DAMAGE TO FLOOR STRUCTURE F/S 1148 BL RIGHT 45 WL 208. REPAIR OF DAMAGE FLOOR STRUCTURE AT F/S1148 BL RIGHT 45 WL 208. FABRICATE REPLACEMENT PARTS AND INSTALL PER SRM.
- [SDR FXGA2022121400512](https://openairdocs.org/sdr/FXGA2022121400512.md): Battery · discharged · Dec 12, 2022 · N794AJ · Boeing 727227 · Smoke Detection
  > CREW RECEIVED A LOWER AFT CARGO FIRE WARNING AT FL360 ON ARRIVAL INTO EFD. CREW IMMEDIATELY INITIATED THE EMERGENCY PROCEDURE AND BEGAN AN EMERGENCY DECENT AND DIVERTED TO CWF, WHICH WAS JUST SOUTH OF POSITION. THE FIRE CREW SWEPT AIRCRAFT UPON LANDING AND NO
- [SDR FXGA20211129001](https://openairdocs.org/sdr/FXGA20211129001.md): Duct · cracked · Nov 27, 2021 · N794AJ · Boeing 727227 · Engine Bleed Air System
  > ON CLIMB APPROXIMATELY 1500' #3 ENGINE HAD FIRE WARNING. ACCOMPLISHED CHECKLIST. LIGHT EXTINGUISHED DID NOT FIRE BOTTLE. RETURNED TO KFLL. ON VISUAL INSPECTION OF ENGINE IT WAS FOUND THAT THE BLEED AIR DUCT HAD RUPTURED/CRACKED.
- [SDR FXGA202103182103](https://openairdocs.org/sdr/FXGA202103182103.md): Stiffener · cracked · Mar 18, 2021 · N794AJ · Boeing 727227 · Wing Miscellaneous Structure
  > L/H WING FRONT SPAR VERTICAL STIFFENER CRACKED AT W/STA 255L. TO REPLACE A CRACKED VERTICAL STIFFENER ON THE LEFT WING FRONT SPAR WEB AT W/STA 254. REPLACE VERTICAL STIFFENER PER EA 20-2021-008. OBTAIN DTA WITHIN 12 MONTHS.
- [SDR FXGA202103182110](https://openairdocs.org/sdr/FXGA202103182110.md): Skin · corroded · Mar 18, 2021 · N794AJ · Boeing 727227 · Elevator, Plate/Skin
  > CORROSION ON L/H ELEVATOR OUTBOARD TRAILING EDGE. TO REPAIR CORRODED ELEVATOR SKIN AT THE TRAILING EDGE IN THE STATIC WICKS AREA. PERFORM REPAIR OF ELEVATOR TRAILING EDGE PER STS ENGINEERING AUTHORIZATION 80-2021-016 AND 80-2021-015. OBTAIN DTA WITHIN 12 MONT
- [SDR FXGA202103042114](https://openairdocs.org/sdr/FXGA202103042114.md): Web · damaged · Mar 4, 2021 · N794AJ · Boeing 727227 · Ailerons
  > DAMAGE WEB AT L/H AILERON TAB HINGE ASSEMBLY. TO PREFORM SPLICE ON A DAMAGED WEB SUPPORTING THE L/H OUTBOARD AILERON TRIM ROD HINGE ASSEMBLY.REMOVE AILERON TRIM ROD HINGE ASSEMBLY. REPAIRE DAMAGE WEB PER B727 SRM 51-40-02 TYPICAL WEB REPAIR. INSTALL AILERON TR
- [SDR FXGA202102022111](https://openairdocs.org/sdr/FXGA202102022111.md): Skin · delaminated · Feb 2, 2021 · N794AJ · Boeing 727227 · Ailerons
  > DELAM ON LH AILERON COMPOSITE TRAILING EDGE. TO REPAIR DELAMINATION ON AILERON TRAILING EDGE. REPAIR AILERON TRAILING EDGE PER B727 SRM 51-40-20 GENERAL REPAIR - ALUMINUM HONEYCOMB REPAIRS - 250 DEGREE FAHRENHEIT (121 DEGREE CELSIUS) CURE.
- [SDR FXGA202102012109](https://openairdocs.org/sdr/FXGA202102012109.md): Stringer · corroded · Feb 1, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORRODED FUSELAGE STRINGER AT F/STA 443, STRINGER 11R. TO REPAIR A CORRODED FUSELAGE STRINGER AT F/STA 443, 11 RIGHT. CUT OUT DAMAGED AREA AND PERFORM REPAIR PER DC-6A&B OVERHAUL MANUAL FIGURE 12-2.
- [SDR FXGA202101062102](https://openairdocs.org/sdr/FXGA202101062102.md): Hinge Fitting · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Leading Edge Devices
  > OUTBOARD HINGE FITTING CORRODED FOR L/H WING #2 LEADING EDGE FLAP AT W/STA 269L. TO REMOVE AND REPLACE A CORRODED FITTING ON #2 LEADING EDGE FLAP (W/STA 269L). REMOVED CORRODED FITTING. MANUFACTURE NEW FITTING PER DRAWINGS NUMBER 65-16271 AND BAC1508-128. INST
- [SDR FXGA202101062101](https://openairdocs.org/sdr/FXGA202101062101.md): Hinge Fitting · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Leading Edge Slat Control System
  > CORRODED HINGE FITTING FOR L/H WING #1 LEADING EDGE FLAP AT W/STA 283L. TO REMOVE AND REPLACE A CORRODED FITTING ON #1 LEADING EDGE FLAP (W/STA 283L). REMOVE CORRODED FITTING. MANUFACTURE NEW FITTING PER DRAWINGS NUMBER 65-16273 AND BAC 1508-128. INSTALL NEW F
- [SDR FXGA202101062106](https://openairdocs.org/sdr/FXGA202101062106.md): Stringer Clip · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORRODED CLIP AT STRINGER 19L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUSELAGE STRINGER 19L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.
- [SDR FXGA202101062104](https://openairdocs.org/sdr/FXGA202101062104.md): Stringer Clip · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORRODED CLIP AT STRINGER 17L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUESLAGE STRINGER 17L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.
- [SDR FXGA202101062105](https://openairdocs.org/sdr/FXGA202101062105.md): Stringer Clip · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORRODED CLIP AT STRINGER 18L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUSELAGE STRINGER 18L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.
- [SDR FXGA2020011392002](https://openairdocs.org/sdr/FXGA2020011392002.md): Support Bracket · cracked · Jan 9, 2020 · N794AJ · Boeing 727227 · Spoilers
  > LEFT WING #3 FLIGHT SPOILER ACTUATOR SUPPORT BRACKETS CRACKED, INBRD AND OUTBRD. REPALACED LEFT WING #3 SPOILER ACTUATOR BRACKETS (BOTH). REMOVED AND REPLACE LEFT WING #3 SPOILER ACTUATOR BRACKETS P/N 65-24608-17 OUTBOARD BRACKET, AND P/N 65-24608-19 INBOARD
- [SDR FXGA201906261920](https://openairdocs.org/sdr/FXGA201906261920.md): Spar · corroded · Jun 26, 2019 · N794AJ · Boeing 727227 · Wing Spar
  > CORROSION ON AFT WING SPAR LOWER CHORD BETWEEN LBBL 19.2 AND WS 210L. CORROSION WAS FOUND ON THE AFT WING SPAR LOWER CHORD CENTER SECTION AND LT SECTION. SPLICES WILL BE PERFORMED AT LBBL 19.2 ON THE CENTER WING SECTION AND AT WS 210 ON THE LT WING SECTION.
- [SDR FXGA201906181949](https://openairdocs.org/sdr/FXGA201906181949.md): Mount · corroded · Jun 18, 2019 · N794AJ · Boeing 727227 · Engine Mount Section
  > REPLACEMENT OF CORODED #2 ENGINE MOUNT FITTING. TO REPLACE CORRODED AFT ENGINE MOUNT FITTING AND TEE CHORDS AT #2 ENGINE POSITION. REMOVE AND REPLACE #2 ENGINE SUPPORT FITTING P/N 65-18670-1, CHORDS P/N 65-31281-3, 65-31281-4, 65-22913-5, 65-22913-6, AND WEB
- [SDR FXGA201906111946](https://openairdocs.org/sdr/FXGA201906111946.md): Door Frame · corroded · Jun 11, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Structure
  > MAIN CARGO DOOR JAMB INNER SKIN REPLACEMENT. TO REPLACE THE MAIN CARGO DOOR JAMB INNER SKIN (FORWARD LOWER SECTION AT F/STA 520) FOR CORROSION DAMAGE. REMOVE AND REPLACE CORRODED SECTIO OF DOOR JAMB PER B727 SRM 51-30-2.
- [SDR FXGA201905241945](https://openairdocs.org/sdr/FXGA201905241945.md): Spar · damaged · May 24, 2019 · N794AJ · Boeing 727227 · Wing Spar
  > CENTER WING SPAR TEMPORARY REPAIR FOR FERRY FLIGHT. TEMPORARY REPAIR FOR DAMAGE TO CENTER WING AFT SPAR LOWER CAP FOR FERRY FLIGHT TO INSTALL PERMANENT REPAIR. 727-227 LEFT HAND WING REPAIR TEMPORARY. S/N 21243.
- [SDR FXGA201905231944](https://openairdocs.org/sdr/FXGA201905231944.md): Skin · corroded · May 23, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Plate/Skin
  > FUESLEAGE SKIN REPLACEMENT BETWEEN F/STA 259.5 AND 360 STRINGER 19L AND 26L. TO REPLACE A CORRODED SKIN BETWEEN F/STA 259.5 AND 360, FROM STRINGER 20L AND 25L. REMOVE AND REPLACE CORRODED SKIN PER SRM.
- [SDR FXGA2019040941932](https://openairdocs.org/sdr/FXGA2019040941932.md): Stringer · corroded · Apr 4, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORRODED FUSELAGE LONGERON #27R F/STA 950. TO REPAIR A CORRODED STRINGER. REMOVE CORROSION AND INSTALL REPAIR PER B727 SRM 51-40-4.
- [SDR FXGA201903081922](https://openairdocs.org/sdr/FXGA201903081922.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON LT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 78.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.
- [SDR FXGA201903081923](https://openairdocs.org/sdr/FXGA201903081923.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 82.5 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.
- [SDR FXGA201903081924](https://openairdocs.org/sdr/FXGA201903081924.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON RT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 88.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.
- [SDR FXGA201903081925](https://openairdocs.org/sdr/FXGA201903081925.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. REMOVE AND REPLACE CORRODED BEAM WITH NEW PER SRM 51-30-2 FASTENER REMOVAL AND INSTALLATION.
- [SDR FXGA201902081912](https://openairdocs.org/sdr/FXGA201902081912.md): Crossbeam · cracked · Feb 8, 2019 · N794AJ · Boeing 727227 · Fuselage Miscellaneous Structure
  > CRACK ON CROSS BEAM STA 856-850 @ LBL 45.50. TO REPAIR A CRACKED WEB ON A FLOOR CROSS BEAM. THE CRACK IS LOCATED BETWEEN F/SAT 850 AND 856 AT LBL 45.50. PERFORM REPAIR OF CRACKED WEB PER REPAIR DRAWING #E2499-001. DTA MUST BE OBTAINED WITHIN 12 MONTHS.
- [SDR FXGA201902041918](https://openairdocs.org/sdr/FXGA201902041918.md): Skin · corroded · Feb 4, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Plate/Skin
  > CORROSION AT RT WING ILLUMINATION LIGHT. TO REPAIR A CORRODED SKIN BETWEEN F/STA 720B AND 720C AND LONGERON S-14R AND S-16R. REPAIR CORRODED SKIN PER SRM 53-30-3 FIGURE 22. SEE PAGE 2 FOR RE-INSPECTION REQUIREMENTS.
- [SDR FXGA201901081901](https://openairdocs.org/sdr/FXGA201901081901.md): Floorbeam · corroded · Jan 8, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON O/B END STA 880 FLOORBEAM LOWER CHORD @ RBL 68. CORROSION ON OUTBOARD END OF STA 880 FLOORBEAM LOWER CHORD AT RBL 68. CUT OUT AND REMOVE DAMAGE, REPAIR PER SRM 53-10-08 FIGURE 8. RE-INSPECTION REQUIREMENTS: HFEC REQUIRED. INITIAL: 55,000 CYCLES
- [SDR FXGA20160226001](https://openairdocs.org/sdr/FXGA20160226001.md): Controller · failed · Feb 25, 2016 · N794AJ · Boeing 727227 · Cabin Pressure Controller
  > AIRCRAFT DEPRESSURIZED IN THE MIDDLE OF A PARABOLA. DESCENT WAS INITIATED AT FIRST INDICATION OF DEPRESSURIZATION. MAXIMUM ALTITUDE REACHED WAS FLIGHT LEVEL 310. FOUND THAT THE CABIN PRESS CONTROLLER HAD FAILED.
- [SDR FXGA20151026001](https://openairdocs.org/sdr/FXGA20151026001.md): Wire Harness · broken · Oct 22, 2015 · N794AJ · Boeing 727217 · Fire Protection System Wiring
  > DURING CRUISE FLIGHT NR 3 ENG FIRE INDICATION. PROCEDURE & CHECKLIST INITIATED. BOTH ENG FIRE BOTTLE DEPLOYED. FIRE INDICATION REMAINED ON. ALL ENG PARAMETERS NORMAL EXCEPT ENG OIL TEMP AT RED LINE. ENG FIRE INDICATION REMAINED ON UP TO SECURING AIRPLANE
- [SDR PCSA2013120501](https://openairdocs.org/sdr/PCSA2013120501.md): Warning Light · illuminated · Dec 4, 2013 · N794AJ · Boeing 727227 · Overheat Detection
  > DURING CLIMB OUT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST & RETURNED TO KTIX.
- [SDR PCSA2012060501](https://openairdocs.org/sdr/PCSA2012060501.md): Engine · power loss · Jun 3, 2012 · N794AJ · Boeing 727227 · Engine (Turbine/Turboprop)
  > DURING CLIMBOUT THE NR 2 ENGINE LOSS POWER.
- [SDR PCSA2011072201](https://openairdocs.org/sdr/PCSA2011072201.md): Hydraulic Line · ruptured · Jul 21, 2011 · N794AJ · Boeing 727227 · Hydraulic System, Auxiliary
  > CLIMBING THROUGH 12000FT B-SYSTEM 2 PUMP LOW PRESS LIGHT FLICKERED FOLLOWED BY A-SYSTEM FLUID DECREASING TO 2.5 GALLONS AND B-SYSTEM FLUID DECREASING TO 0. APPROPRIATE CHECKLIST INITIATED AND RETURNED TO BASE WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED.
- [SDR PCSA2011060901](https://openairdocs.org/sdr/PCSA2011060901.md): Regulator Valve · leaking · Jun 7, 2011 · N794AJ · Boeing 727227 · Hydraulic Reservoir, Main
  > DURING PARABOLA NUMBER 2 STRONG SMELL IN FLIGHT DECK AND CABIN AFTER NUMBER 5. COULD NOT IDENTIFY AND RETURNED TO BASE. MAINTENANCE FOUND THE SMELL TO BE SKYDROL FROM THE HYDRAULIC RESERVOIR PRESSURE REGULATOR LEAKING INTO THE PRESSURIZING LINE. THE LINES W
- [SDR PCS2008F00000](https://openairdocs.org/sdr/PCS2008F00000.md): Compressor · failed · Aug 26, 2008 · N794AJ · Boeing 727227 · Turbine Engine Compressor Section
  > DURING CLIMB BETWEEN 180 TO 210 FLIGHT LEVEL NR 1 ENG COMPRESSOR STALL FOLLOWED BY OIL TEMP RISE. AFTER SECOND COMPRESSOR STALL NR 1 ENG OIL PRESS LIGHT ILLUMINATED. ENG WAS SHUT DOWN PER AOM. NR 1 ENG OPERATED APPROX 9 MINUTES OIL PRESS ABOUT 20 PSI. POST
- [SDR PCSA9210601](https://openairdocs.org/sdr/PCSA9210601.md): Detection Sys · false indication · Sep 21, 2006 · N794AJ · Boeing 727227 · Overheat Detection
  > FLIGHT 819 DEPARTED FROM MIA, WHILE IN CRUISE AT THE ASSIGNED ALTITUDE (ONE HOUR OUT) THE CREW REPORTED THE NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED, THE CREW PERFORMED THE ABNORMAL PROCEDURES, THE NUMBER 3 STRUT OVERHEAT LIGHT WENT OUT. THE AIRCRAFT RETURN
- [SDR PCSA8180601](https://openairdocs.org/sdr/PCSA8180601.md): Actuator · bypassing · Aug 18, 2006 · N794AJ · Boeing 727227 · Landing Gear Door Retract Section
  > FLIGHT 8413 DEPARTED MIA WHILE IN THE CLIMB THE CREW REPORTED THE LEFT HAND MAIN LANDING GEAR DOOR WARNING LIGHT CAME ON AFTER THE LANDING GEAR SELECTOR HANDLE WAS MOVED FROM THE GEAR UP POSITION TO THE OFF POSITION. THE AIRCRAFT RETURNED BACK TO MIA AND LAND
- [SDR PCSA0526051](https://openairdocs.org/sdr/PCSA0526051.md): Pcu · malfunctioned · May 26, 2005 · N794AJ · Boeing 727227 · Elevator Control System
  > ON TAXI OUT CONTROL YOKE JAMMED WILL NOT MOVE FWD. AC RETURNED TO RAMP. AIRCRAFT WAS FERRIED BACK TO MIAMI. NO DEFECTS REPORTED ON FLIGHT. REMOVED FLOOR PANEL, INSPECTED CONTROL CABLES EBL, EAL, EBR, EAR & PULLEYS BS 540, 740, 870, 950 & 1050 NO DEFECTS.
- [SDR 2004F00304](https://openairdocs.org/sdr/2004F00304.md): Chip Detector · missing · Jun 17, 2004 · N794AJ · Boeing 727227 · Turbine Engine Oil System
  > EN ROUTE TO MEXICO, THE NR 2 OIL QUANTITY DECREASED TO ZERO FOLLOWED BY A DROP IN OIL PRESSURE. PRECAUTIONARY SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED BACK TO MMMD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AND FOUND NR 4 BEARING
- [SDR 2004F00243](https://openairdocs.org/sdr/2004F00243.md): Engine · malfunctioned · Oct 27, 2003 · N794AJ · Boeing 727227 · Turbine Engine Oil System
  > FLT 813 - KMIA-TBPB - AFTER DEPARTURE FORM KMIA, NR 3 OIL PRESSURE INDICATED ABOVE ARC LINE, AND THEN OIL TEMP BEGAN CLIMBING AND WENT ABOVE ARC LINE. SHUT OFF NR 3 ENGINE AS PER PROCEDURES. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR 2003F00555](https://openairdocs.org/sdr/2003F00555.md): Fuel Control · contaminated · Aug 24, 2003 · N794AJ · Boeing 727227 · Fuel Control/Turbine Engines
  > AFTER DEPARTURE FROM KMIA, NR 1 ENGINE RPM BEGAN TO INCREASE AND DECREASE DURING CLIMB OUT. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAITNENANCE INSPECTED NR 1 ENGINE INLET AND EXHAUST IAW CHAPTER 71-00. NO DAMAGE FOUND, INSPECTED
- [SDR 2003F00298](https://openairdocs.org/sdr/2003F00298.md): Blade · damaged · Mar 17, 2003 · N794AJ · Boeing 727227 · Turbine Engine Compressor Section
  > IN FLIGHT NR 3 ENGINE COMPRESSOR STALLED TWICE AND HAD HIGH EGT INDICATION. ENGINE NR 3 WAS SHUTDOWN IN FLIGHT AND FLIGHT CONTINUED TO KMIA WITHOUT FURTHER INCIDENT. MIA MAINTENANCE INSPECTED ENGINE NR 3 AND FOUND THE C-9 THROUGH C-13 BLADES DAMAGED. ENGNE
- [SDR 2003F00316](https://openairdocs.org/sdr/2003F00316.md): Oil Cap · loose · Feb 26, 2003 · N794AJ · Boeing 727227 · Turbine Engine Oil System
  > FLT 835 - KMIA/UVF - CAPTAIN REPORTED, NR 2 ENGINE OIL QUANTITY INDICATED 1.5 WHILE INFLIGHT. LOW OIL QUANTITY LIGHT DID NOT ILLUMINATE. AIRCRAFT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE OIL CAP NOT SECURED. ENGINE
- [SDR COOSDR02201](https://openairdocs.org/sdr/COOSDR02201.md): Door Frame · cracked · Jul 1, 2002 · N794AJ · Boeing 727227 · Fuselage Main, Structure
  > LEFT MAIN LANDING GEAR, WING DOOR AFT FRAME CRACKED.
- [SDR COOSDR020198](https://openairdocs.org/sdr/COOSDR020198.md): Floorbeam · corroded · Jul 1, 2002 · N794AJ · Boeing 727227 · Fuselage Main, Floor Beam
  > MAIN CARGO CABIN BS 1130 LOWER CHORD CORRODED.
- [SDR COOSDR020192](https://openairdocs.org/sdr/COOSDR020192.md): Structure · delaminated · Jul 1, 2002 · N794AJ · Boeing 727227 · Leading Edge Devices
  > RIGHT WING OUTBOARD FORE FLAP (PN 65-21631-274) (SN BN386) UPPER SKIN AND HONEYCOMB CORE DELAMINATED SECTION.
- [SDR COOSDR020191](https://openairdocs.org/sdr/COOSDR020191.md): Structure · delaminated · Jul 1, 2002 · N794AJ · Boeing 727227 · Leading Edge Devices
  > LEFT WING INBOARD FORE FLAP (PN 652130-188) (SN BN720) UPPER, LOWER SKIN AND HONEYCOMB CORE DELAMINATED SECTION.
- [SDR COOSDR020190](https://openairdocs.org/sdr/COOSDR020190.md): Access Panel · delaminated · Jul 1, 2002 · N794AJ · Boeing 727227 · Air Conditioning Doors
  > AIR CONDITION BAY ACCESS PANEL (PN 65-58513-12) INNER SKIN DELAMINATED.
- [SDR COOSDR020189](https://openairdocs.org/sdr/COOSDR020189.md): Structure · corroded · Jul 1, 2002 · N794AJ · Boeing 727227 · Trailing Edge Flaps
  > RIGHT WING INBOARD AFT FLAP (PN 65-21634-80) (SN BN375) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR0220188](https://openairdocs.org/sdr/COOSDR0220188.md): Skin · delaminated · Jul 1, 2002 · N794AJ · Boeing 727227 · Trailing Edge Flaps
  > LEFT WING OUTBOARD AFT FLAP (PN 65-21635-85) (SN BN486) UPPER AND LOWER SKIN DELAMINATED.

Next page: https://openairdocs.org/aircraft/N794AJ/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 = 'N794AJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N794AJ/reports

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