# Service difficulty reports: N708AA

A list on [N708AA](https://openairdocs.org/aircraft/N708AA.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 · 80 reports

- [SDR C8GA2011000028](https://openairdocs.org/sdr/C8GA2011000028.md): Proximity Switch · faulted · Dec 8, 2011 · N708AA · Boeing 727223 · Landing Gear Position and Warning
  > DURING CLIMB, ON GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. THE GEAR LEVER WAS CYCLED TO THE OFF POSITION, RED NOSE LIGHT REMAINED ILLUMINATED WITH THE GREEN NOSE GEAR DOWN LOCK LIGHT ILLUMINATED. THE ACFT RETURNED TO DEPARTURE AND LANDED WI
- [SDR C8GA201111150025](https://openairdocs.org/sdr/C8GA201111150025.md): Transceiver · failed · Nov 15, 2011 · N708AA · Boeing 727223 · Weather Radar System
  > DURING CRUISE, THE WEATHER RADAR SCREEN WENT BLANK. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING THAT THE RADAR TRANSCEIVER TO BE AT FAULT. R & R THE RADAR TRANSCEIVER AND PERFORMED OPS CHECKS WITHOUT DE
- [SDR FOTR2021700540](https://openairdocs.org/sdr/FOTR2021700540.md): Skin · corroded · Jan 26, 2011 · N708AA · Boeing 727223 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON RT HORIZ STAB UPPER T/E SKIN AT NR 3 ELEVATOR HINGE CUTOUT. REMOVED CORROSION ON RT HORIZ STAB T/E BEAM WITH 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1 AND 55-10-1. FITTED NEW BEAM PN 65-24571-2, SN BN574 AND LOCATED HOL
- [SDR FOTR2021700137](https://openairdocs.org/sdr/FOTR2021700137.md): Hinge · cracked · Jan 26, 2011 · N708AA · Boeing 727223 · Fuselage, Door Hinge
  > UPPER HINGE AFT MOST SEGMENT HAS AFT LOBE CRACKED. REMOVED AFT HINGE SEGMENT IAW SRM 51-30-2 AND 200F MM CH 52, FIG 5210B. FABRICATED NEW HINGE SEGMENT FROM MS20001-16-7200 PO 2021728 DIM 18" LONG. INSTALLED NEW HINGE SEGMENT IAW SRM 51-30-2 AND 51-10-2 AND
- [SDR FOTR2021700257](https://openairdocs.org/sdr/FOTR2021700257.md): Angle · cracked · Jan 26, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > RT WHEELWELL VERTICAL ANGLE IS CRACKED AT BS 870, RBL 8 BELOW LOAD CONTROL VALVE. REMOVED SUPPORT STRUCTURE AND VERTICAL ANGLE AT BS 870, RBL 8 FOR REPAIR IAW SRM 51-30-2. REPAIRED BS 870 WEB IAW SRM 53-10-9, FIG 5. FABRICATED 4 EA REPAIR FILLERS FROM 202
- [SDR FOTR2021700544](https://openairdocs.org/sdr/FOTR2021700544.md): Skin · corroded · Jan 26, 2011 · N708AA · Boeing 727223 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON LT HORIZ STAB UPPER SKIN AT NR 4 ELEVATOR HINGE CUTOUT. REMOVED CORROSION ON LT HOR STAB T/E SKIN BEAM AT NR 4 HINGE CUTOUT. MEASURED.040" MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1, 51-10-6 AND 55-10-1. REMOVED LT HORIZ STAB T/E
- [SDR FOTR2021700623](https://openairdocs.org/sdr/FOTR2021700623.md): Stringer · damaged · Jan 26, 2011 · N708AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > STA 540 AT STR 18R HAS HOLE DRILLED THRU RADIUS OF STRINGER. CUT OUT DAMAGED STRINGER DIM 19.5" LONG FROM STR 18R. FABRICATED NEW STRINGER SECTION FROM BAC1498-141 FROM 7075T6, PO 20041102, DIM 19.5", FABRICATED NEW TOP HAT FROM BAC1498-131, PO 90010803, DIM
- [SDR FOTR2021700212](https://openairdocs.org/sdr/FOTR2021700212.md): Attach Bracket · cracked · Jan 26, 2011 · N708AA · Boeing 727223 · Wing, Attach Fittings
  > LT WING NR 2 SLAT ACTUATOR, INBD ATTACH BRACKET IS CRACKED. SLAT STA 291.0 REMOVED SLAT ACTUATOR SUPPORT STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STIFFENER FROM BAC1503-100145 PO NR 20217147 DIM 9" X 4.5" AND SHIM FROM 7075T6.032" PO NR 9006027 DIM 5" X
- [SDR FOTR2021700805](https://openairdocs.org/sdr/FOTR2021700805.md): Structure · damaged · Jan 25, 2011 · N708AA · Boeing 727223 · Nacelle/Pylon, Main Frame
  > NR 3 PYLON DAMAGED. REMOVED TITANIUM DOUBLER FROM NR 3 PYLON IAW SRM 51-30-2 AND EA 2708-5401 REV 1, LOCATED AND DRILLED NEW TITANIUM DOUBLER PN 69-18227-2, PO 20217102 IAW SRM 51-30-5 AND 51-30-6. FABRICATED 2 EA, FREEZE PLUGS FROM 15-5PH.375 PO 20217121 DI
- [SDR FOTR20217842](https://openairdocs.org/sdr/FOTR20217842.md): Fitting · corroded · Jan 25, 2011 · N708AA · Boeing 727223 · Fuselage Main, Attach Fittings
  > FUSELAGE EXTERIOR BS 740 PRESSURE FITTING IS CORRODED BETWEEN STR 27L-28L. REMOVED FITTING FROM STA 740 IAW SRM 51-30-2, FORMED FITTING FROM 7075-0, 7.2" X 10.7".190" PO 2905745 IAW SRM 51-20-1, FIG 7. HEATED TREATED FITTING TO 7075T6 IAW ENG REPORT 2-37153-
- [SDR FOTR/2021700365](https://openairdocs.org/sdr/FOTR%2F2021700365.md): Fairing · gouged · Jan 25, 2011 · N708AA · Boeing 727223 · Trailing Edge Flaps
  > RT WING, OTBD FLAP, MID FLAP OTBD FAIRING HAS 2 EA GOUGES AND 1 EA LOOSE FASTENER. CUTOUT DAMAGED AREA DIM 1.5" X.6" IAW SRM 57-20-4, FIG 1. FABRICATED 2 EA REPAIR DOUBLERS FROM 2024-T3.050" PO 90010715 DIM 5.6250" X 2.7500" AND 4.7" X 2". FABBED REPAIR
- [SDR FOTR2021700828](https://openairdocs.org/sdr/FOTR2021700828.md): Frame · damaged · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) MAIN CABIN FRAME AT BS 720A BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLE. CUTOUT DAMAGED AREA, DIMENSION 1" X.75" IAW SRM 51-10-1. FABRICATED DOUBLER FROM 7075-T6 PO 90010361,.063" DIMENSION 5.8750" X 3.8750" IAW SRM 51-40-3, FIG 1. INSTALLED REPAIR P
- [SDR FOTR/20217/00827](https://openairdocs.org/sdr/FOTR%2F20217%2F00827.md): Frame · damaged · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) MAIN CABIN FRAME AT BS 700 BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLES. CUTOUT DAMAGED AREA AT BS 700 DIMENSION 1" X.8" IAW SRM 51-10-1. FABRICATED DOUBLER FROM 7075-T6.063 PO 90010361, DIMENSION 6.8750" X 3.5" IAW SRM 51-40-3, FIG 1. INSTALLED REPAI
- [SDR FOTR/20217/00826](https://openairdocs.org/sdr/FOTR%2F20217%2F00826.md): Frame · damaged · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) CABIN FRAME AT BS 680 BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLES. CUTOUT DAMAGED AREA DIMENSION 1.4" X.6" ON BS 680 BETWEEN STRINGER 16L-17L IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR ANGLE FROM 7075-T6.050" PO 9009353 DIMENSION 7" X 3.6" IAW SRM
- [SDR FOTR2021700821](https://openairdocs.org/sdr/FOTR2021700821.md): Frame · dented · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) CABIN FRAME AT BS 560 BETWEEN STR 15R-16R DENTED. CUTOUT DAMAGED AREA ON BS 560 BETWEEN STR 15R-16R, DIMENSION 1.1" X 1.1" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR ANGLE FROM 7075-T6.071' PO 9009519, DIMENSION 6.5" X 3.5" AND REPAIR FILLER FROM 7075-
- [SDR FOTR2021700725](https://openairdocs.org/sdr/FOTR2021700725.md): Seat Track · corroded · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > (FOTR) MAIN CABIN CARGO DECK, AT BS 560-580 LBL 45 INBD SIDE OF SEAT TRACK FLANGE HAS CORROSION. REMOVED CORROSION ON CABIN SEAT TRACK LBL 45, BS 560-580 IAW SRM 51-10-1, FOUND OUT OF LIMITS. REMOVED SEAT TRACK FROM BS 480-689 IAW SRM 51-30-2. FABRICATED SEA
- [SDR FOTR2021700682](https://openairdocs.org/sdr/FOTR2021700682.md): Seat Track · corroded · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > (FOTR) LT FUSELAGE CABIN INTERIOR, HAS SURFACE CORROSION ON SEAT TRACK FLANGE BETWEEN BS 720A-720D, LBL 24. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FABRICATED NEW SEAT TRACK FROM BAC1520-792 7178-T6511 PO 90010776 DIMENSION 17'1.7500"
- [SDR FOTR202170064](https://openairdocs.org/sdr/FOTR202170064.md): Frame · dented · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) LT FUSELAGE CABIN INTERIOR HAS FRAME DENTED AT BS 720, STR 16L. CUTOUT DAMAGED AREA ON FRAME DIMENSION 9" X.9" AT BS 720, STR 16L IAW SRM 51-10-1. FABRICATED FRAME REPAIR FROM 7075-T6.063" PO 90010361, DIMENSION 5.5" X 17.3" IAW SRM 51-40-3, FIG 1. T
- [SDR FOTR2021700661](https://openairdocs.org/sdr/FOTR2021700661.md): Frame · cracked · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) REMOVED DAMAGED AREA FROM FRAME AT STR 17L DIMENSION 2.2500" X 1.5" IAW SRM 51-10-1, AND 51-30-2. FABRICATED REPAIR IAW SRM 51-40-3 FROM 7075-0 DIMENSION 9.1" X 4.1" PO 20198132. HEAT TREATED TO 7075T6 IAW FASI REPORT 2-37153-801A. FABRICATED CLIP FRO
- [SDR FOTR2021700658](https://openairdocs.org/sdr/FOTR2021700658.md): Stringer · gouged · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > (FOTR) FUSELAGE CABIN INTERIOR HAS GOUGE AT FRAME BS 360 STR 6L. CUTOUT DAMAGED AREA AT STR 6L BS 360, DIMENSION 9.8750" FABRICATED STR FILLER FROM BAC 1498-143-7075T6 DIMENSION 9.8750". FABRICATED STRAP PLATES NR1 (1 EA) FROM 2024T3.250" DIMENSION.8" X 1
- [SDR FOTR2021700656](https://openairdocs.org/sdr/FOTR2021700656.md): Intercostal · cracked · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > (FOTR)FUSELAGE CABIN INTERIOR, INTERCOSTAL IS CRACKED AT STR 16L BETWEEN BS 348-360. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR FROM 2024-T3.063 PO 90010689, DIMENSION 5" X 3" IAW SRM 51-40-2. TREATED AND PRIMED IAW SRM 51-10
- [SDR FOTR2021700653](https://openairdocs.org/sdr/FOTR2021700653.md): Shear Tie · cracked · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Internal Mounting Structure
  > (FOTR) FUSELAGE CABIN INTERIOR, HAS CRACK INDICATION ON SHEARTIE, STR 8R BS 1130. REMOVED FASTENERS AT FUSELAGE FRAME IN MAIN CABIN BS 1130 STR 8R IAW SRM 51-30-2. C/W HFEC INSP IAW NDTM 51-00-00, FIG 23, PART 6. NO CRACKS NOTED. CUT SHEARTIE DIMENSION 6.2' X
- [SDR FOTR2021700651](https://openairdocs.org/sdr/FOTR2021700651.md): Web · cracked · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > (FOTR) CABIN INNER WEB DENTED AT BS 640, STR 6L. (AFT MAIN CARGO DOOR). C/W HFEC ON WEB IAW NDTM 51-00-00 FIGURE 23, PART 6. CRACK FOUND. REMOVED TRIM PANEL FROM BS 520-600, REMOVED AFT UPPER INNER SKIN FROM BS 600-560. FABRICATED NEW INNER SKIN FROM 2024-T3.
- [SDR FOTR2021700631](https://openairdocs.org/sdr/FOTR2021700631.md): Skin · dented · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > (FOTR) AFT LOWER FUSELAGE EXTERIOR SKIN LT SIDE AT STATION 1148-1160 AND BETWEEN STR 25L-26L, SKIN IS DENTED. CUT DAMAGED AREA OUT OF UPPER LAP SKIN DIMENSION 4.5" X 5.5". FABRICATED REPAIR FILLER FROM 2024-T3.063 PO 90010580 DIMENSION 12" X 14". FABRICATED
- [SDR FOTR2021700626](https://openairdocs.org/sdr/FOTR2021700626.md): Stringer · corroded · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > (FOTR) STR 27L BETWEEN BS 720F-740 IS CORRODED. CUT DAMAGED STR DIMENSION 12" LONG IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR STR FROM BAC1498-147 7075T62 PO 2014059 DIMENSION 11.4375" LONG AND FABRICATED REPAIR STR SPLICE FROM BAC1498-131 7075-T6 PO90010803 DI
- [SDR FOTR/20217/00507](https://openairdocs.org/sdr/FOTR%2F20217%2F00507.md): Intercostal · dented · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > (FOTR) C1 DOOR CUTOUT INTERCOSTAL IS DENTED AT UPPER FLANGE BS 627 BETWEEN STR 24R-25R. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-30-2. LOCATED AND DRILLED NEW INTERCOSTAL PN 65-56101-36, PO 2021752. AND INSTALLED AT BS 627 BETWEEN STR 24R-25R IAW SRM 51-30-2,5
- [SDR FOTR/20217/00381](https://openairdocs.org/sdr/FOTR%2F20217%2F00381.md): Frame · dented · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) CABIN FRAME DENTED AT BS 400 BETWEEN STRINGER 5R-6R. REMOVED DAMAGED AREA OF BS 400 FRAME AT STR 5R-6R DIMENSION 2.25" X 4" IAW SRM 53-10-4 FIG 1, FABRICATED REPAIR FILLER AND 2 EACH SPLICES FROM 7075-0,.050, PO 90010501 AND HEAT TREATED TO T-6 IAW S
- [SDR FOTR/20217/00378](https://openairdocs.org/sdr/FOTR%2F20217%2F00378.md): Frame · dented · Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
  > (FOTR) CABIN FRAME AT BS 380 DENTED BETWEEN STR 5R-6R, REMOVED DAMAGE AREA OF BS 380 FRAME AT STR 5R-6R, DIMENSION 15" X 4" IAW SRM 53-10-4, FIG 1. FABBRICATED REPAIR FRAME AND 2 EACH SPLICES FROM 7075-0.050 PO 90010501 AND HEAT TREATED TO T-6 IAW SRM 53-10-0
- [SDR ABXR201006050003](https://openairdocs.org/sdr/ABXR201006050003.md): Attach Angle · corroded · Jun 5, 2010 · N708AA · Boeing 727223 · Fuselage Main, Attach Fittings
  > DURING THE ACCOMPLISHMENT OF A ROUTINE CPCP INSP CARD, A FAIRING ATTACH ANGLE WAS FOUND CORRODED BEYOND LIMITS. THE CORROSION DAMAGE WAS R & R WITH AN ANGLE FABRICATED FROM 0.050" 7075 T6 IAW THE SRM. THE ITEM WAS RETURNED TO SERVICE.
- [SDR C8GA201000004](https://openairdocs.org/sdr/C8GA201000004.md): Duct · separated · Mar 4, 2010 · N708AA · Boeing 727223 · Engine Cooling System
  > FLT 2739 FROM ATL TO TOL. DURING CLIMB OPERATION AN AIRFRAME VIBRATION WAS NOTED AND ISOLATED TO THE NR 2 ENGINE. AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. IT WAS NOTED THAT THE 8TH STAGE DUCT SEPARATE
- [SDR C8GA20090182](https://openairdocs.org/sdr/C8GA20090182.md): Indicator · erratic · Aug 28, 2009 · N708AA · Boeing 727223 · Airspeed/Mach Indicator
  > DURING TAKEOFF ROLL THE CAPTAINS AIRSPEED INDICATOR BEGAN TO CYCLE FROM 0-300 KNOTS. THE TAKEOFF WAS ABORTED WHERE THE CREW RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND THE CAPTAINS AIRSPEED INDICATOR WAS REMOVED AND REPLACED. OPS C
- [SDR C8GA20090004](https://openairdocs.org/sdr/C8GA20090004.md): Linkage · damaged · Feb 3, 2009 · N708AA · Boeing 727223 · Leading Edge Slat Position Indicating System
  > FLT 1716 FROM TOL TO STL. DURING CLIMB OPERATION WHEN RETRACTING THE FLAP FROM 5 DEGREES TO 2 DEGREES THE NR 4 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED.
- [SDR C8GA20090003](https://openairdocs.org/sdr/C8GA20090003.md): Position Switch · inoperative · Feb 3, 2009 · N708AA · Boeing 727223 · Leading Edge Slat Position Indicating System
  > FLT 2715 FROM IAH TO TOL. DURING CLIMB OPERATION WHEN RETRACTING THE FLAP FROM 5 DEGREES TO 2 DEGREES THE NR 4 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED.
- [SDR C8GA20080065](https://openairdocs.org/sdr/C8GA20080065.md): Fire Loop · shorted · Dec 19, 2008 · N708AA · Boeing 727223 · Fire Detection
  > FLT 716. ON DECENT THE APU FIRE LIGHT ILLUMINATED AND THE MASTER FIRE BELL SOUNDED. THE APPROPRIATE CHECKLIST ACCOMPLISHED. THE APU FIRE BOTTLE WAS DISCHARGED. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT T
- [SDR C8GA20080031](https://openairdocs.org/sdr/C8GA20080031.md): Slat · malfunctioned · Oct 28, 2008 · N708AA · Boeing 727223 · Leading Edge Slat Control System
  > FLT 715 FROM MEM TO TOL. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 7 LEADING EDGE DEVICE WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION OF THE NR 7 LEADING EDGE POSITION SWITCH WAS PERFORMED A
- [SDR G8G2008F00001](https://openairdocs.org/sdr/G8G2008F00001.md): Fitting · faulty · Jun 11, 2008 · N708AA · Boeing 727223 · Engine Oil System (Airframe Furnished)
  > DURING CLIMB, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND OIL FILTER BYPASS SWITCH GEARBOX FITTING
- [SDR C8GA200800](https://openairdocs.org/sdr/C8GA200800.md): Fitting · damaged · Jun 11, 2008 · N708AA · Boeing 727223 · Nacelle/Pylon, Attach Fittings
  > FLT 720 FROM TOL TO MCO. DURING CLIMB OPERATION OUT OF TOL THE NR 2 ENG LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE ACFT LANDED IN TOL WITHOUT INCIDENT. POST FLIGHT INSPECTIO
- [SDR C8G2008F00003](https://openairdocs.org/sdr/C8G2008F00003.md): Fitting · loose · Jun 11, 2008 · N708AA · Boeing 727223 · Turbine Engine Oil System
  > DURING CLIMB OPERATION, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENG WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AC LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 2 ENGINE OIL FILTER BYPASS SW
- [SDR C8GA20080013](https://openairdocs.org/sdr/C8GA20080013.md): Overheat Loop · faulted · Apr 1, 2008 · N708AA · Boeing 727223 · Overheat Detection
  > CLT TO BNA - DURING CLIMB OPERATION, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 STRUT OVERHEAT DETECTOR LOOP AT FAULT. REMOVED AND REPLACED N
- [SDR C8GA20070004](https://openairdocs.org/sdr/C8GA20070004.md): Gearbox · leaking · Mar 20, 2007 · N708AA · Boeing 727223 · Turbine Engine Accessory Drive
  > FLT 715 FROM HRL TO MEM. DURING CRUISE OPERATION NR 2 LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A DECREASE IN OIL PSI AND OIL QUANTITY. PERFORMED APPROPRIATE CHECKLIST AND SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED TO IAH WHERE IT LANDED WITHOUT INCIDENT. POS
- [SDR C8GA20060015](https://openairdocs.org/sdr/C8GA20060015.md): Door · jammed · Sep 13, 2006 · N708AA · Boeing 727223 · Passenger/Crew Doors
  > ON CLIMB, AIRCRAFT WOULD NOT PRESSURIZE NORMALLY. CREW NOTED SQUEAL AT L1 DOOR. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND L1 DOOR JAMMED. OPENED AND INSPECTED L1 DOOR. CYCLED DOOR SEVERAL TIMES. OPS CHECK GOOD. AIRCRAFT PRESSURIZES NORMALLY.
- [SDR C8GA20060012](https://openairdocs.org/sdr/C8GA20060012.md): Door Seal · out of adjust · Sep 6, 2006 · N708AA · Boeing 727227 · Cabin Pressure Control System
  > FLT 1712 FROM TOL TO DEN. DURING CLIMB PASSING THROUGH APPROXIMATELY 4000 FT CREW HEARD A LOUD SQUEAL ACCOMPANIED BY FLUCTUATING PRESSURIZATION. AIRCRAFT RETURNED TO TOL WERE IT LANDED WITHOUT INCIDENT. FOUND L1 DOOR UPPER HINGE COVER TO BE AT FAULT, REPOSI
- [SDR C8GA20060010](https://openairdocs.org/sdr/C8GA20060010.md): Window · failed · Aug 4, 2006 · N708AA · Boeing 727200 · Flight Compartment Windows
  > FLT 705 FROM YYC TO MSP. ON CLIMB, AT APPROXIMATELY FL30.0, AIRCRAFT EXPERIENCED SEVERE TURBULENCE AND HAIL DAMAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO YYC. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE RADOME WITH APPROXIMATELY 24 INCH DIAMETER HOLE
- [SDR C8GA20060008](https://openairdocs.org/sdr/C8GA20060008.md): Warning Light · false activation · Jun 20, 2006 · N708AA · Boeing 727223 · Overheat Detection
  > FLT 711 FROM DEN TO TOL. DURING CLIMB THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHICH WAS EXTINGUISHED ONLY BY REDUCING THE NR 2 ENGINE THROTTLE TO IDLE. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, TROUBLE
- [SDR C8GA20060007](https://openairdocs.org/sdr/C8GA20060007.md): Oil Cooler · inoperative · Jun 16, 2006 · N708AA · Boeing 727223 · Engine Oil Cooler
  > FLT 1711 FROM LAX TO TOL. DURING CLIMB PASSING THROUGH 10,000FT THE NR 3 ENGINE CSD TRIPPED INDICATING 140 DEGREE'S CELSIUS IN TEMP. THE NR 2 ENGINE CSD WENT TO 140 DEGREE'S AND NR 1 CSD WAS OPERATING HOT AT 125 DEGREE'S. AIRCRAFT DIVERTED TO SAN AND LANDE
- [SDR C8GA20060003](https://openairdocs.org/sdr/C8GA20060003.md): Connector · contaminated · Feb 28, 2006 · N708AA · Boeing 727223 · Electrical Power System Wiring
  > FLT 1059 FROM TOL TO MCI, DURING CLIMBOUT NR 3 ENGINE EPR GAUGE AND F/O'S AIRSPEED INDICATOR CEASED OPERATION FOLLOWED BY FLAGS ON F/O'S SIDE, BOTH FLIGHT RECORDER AND NR 2 COMPUTER C/B'S TRIPPED AND WOULD NOT RESET. AIRCRAFT RETURNED TO TOL WITHOUT INCIDENT.
- [SDR C8GA20050024](https://openairdocs.org/sdr/C8GA20050024.md): Door · open · Dec 2, 2005 · N708AA · Boeing 727223 · Passenger/Crew Doors
  > DURING CLIMBOUT OPERATION, AIRCRAFT WOULD NOT PRESSURIZE ABOVE 1.5 PSID. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND L1 ENTRY DOOR NOT FULLY CLOSED, OPEN, CYCLED AND RESET DOOR, CONFIRMED FULLY CLOSED AND LOCKED. NO DEFECTS NOTED. AIRC
- [SDR C8GA20040019](https://openairdocs.org/sdr/C8GA20040019.md): Engine · damaged · Sep 16, 2004 · N708AA · Boeing 727223 · Engine (Turbine/Turboprop)
  > FLT 727 FROM DFW TO TOL. ON TAKEOFF, THE NR 3 ENGINE HAD STRONG VIBRATION. IN-FLIGHT SHUTDOWN OF THE NR 3 ENGINE AS A PRECAUTIONARY ADVISED ATC DECLARED EMERGENCY AND AIR TURN BACK TO DFW. AIRCRAFT WAS INSPECTED AND FOUND FAILURE OF TURBINE SECTION PER EVIDE
- [SDR C8GA20040007](https://openairdocs.org/sdr/C8GA20040007.md): Toggle · bent · Jun 17, 2004 · N708AA · Boeing 727223 · Trailing Edge Flap Control System
  > AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO KBOS. NO EMERGENCY ACTION WAS TAKEN AND AIRCRAFT LANDED WITHOUT INCIDEN
- [SDR C8GA20030005](https://openairdocs.org/sdr/C8GA20030005.md): Downlock · defective · Feb 27, 2003 · N708AA · Boeing 727223 · Landing Gear Position and Warning
  > FLIGHT 705 FROM KMSP TO KTOL. ON APPROACH INTO TOLEDO, THE LEFT HAND MAIN GEAR INDICATED UNSAFE RED LIGHT ON. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-06-4. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE LEFT HAND GEA

Next page: https://openairdocs.org/aircraft/N708AA/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 = 'N708AA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N708AA/reports

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